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Aerodynamics, Supersonic
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The concept ** Aerodynamics, Supersonic** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

The Resource
Aerodynamics, Supersonic
Resource Information

The concept

**Aerodynamics, Supersonic**represents the subject, aboutness, idea or notion of resources found in**University of Oklahoma Libraries**.- Label
- Aerodynamics, Supersonic

## Context

Context of Aerodynamics, Supersonic#### Subject of

- A Method for determining the aerodynamic characteristics of two- and three-dimensional shapes at hypersonic speeds
- A Program for computing steady inviscid three-dimensional supersonic flow on reentry vehicles : volume I : analysis and programming
- A System for aerodynamic design and analysis of supersonic aircraft
- A System for aerodynamic design and analysis of supersonic aircraft
- A combined aerodynamic and guidance approach for a simple homing system
- A computational system for aerodynamic design and analysis of supersonic aircraft : part 1-general description and theoretical development
- A computational system for aerodynamic design and analysis of supersonic aircraft : part 3-computer program description
- A fine-wire stagnation temperature probe
- A finite difference solution for the propagation of sound in near sonic flows
- A method for designing low-drag nose-inlet-body combinations for operation at moderate supersonic speeds
- A method of characteristics computer program for the solution of supersonic flow fields about axially symmetric bodies
- A modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack
- A pivoting-cowl-and-spike technique for efficient angle-of-attack operation of supersonic inlets
- A pressure-distribution investigation of a supersonic-aircraft fuselage and calibration of the Mach number 1.40 nozzle of the Langley 4- by 4-foot supersonic tunnel
- A sensitivity equation approach to shape optimization in fluid flows
- A study of the sonic-boom characteristics of a blunt body at a Mach number of 4.14
- A study of the sonic-boom characteristics of a blunt body at a Mach number of 6
- A thin wing in a compressible flow
- A wind-tunnel test technique for measuring the dynamic rotary stability derivatives including the cross derivatives at high Mach numbers
- A wing concept for supersonic maneuvering
- Accuracy of approximate methods for predicting pressures on pointed nonlifting bodies of revolution in supersonic flow
- Aerodynamic characteristics and flying qualities of a tailless triangular-wing airplane configuration as obtained from flights of rocket-propelled models at transonic and low supersonic speeds
- Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch at M = 2.0
- Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail
- Aerodynamic characteristics of a Sparrow III missile model in the flow field of a generalized parent body at Mach 2.86
- Aerodynamic characteristics of a distinct wing-body configuration at Mach 6 : experiment, theory, and the hypersonic isolation principle
- Aerodynamic characteristics of a fixed arrow-wing supersonic cruise aircraft at Mach numbers of 2.30, 2.70, and 2.95
- Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ÌŠswept double-delta wing at Mach number 0.2
- Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47
- Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2Â° delta wing and an unswept horizontal tail
- Aerodynamic heating of a cone in supersonic flight
- Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base
- Aerodynamic test and analysis of a turbojet-boosted launch vehicle concept (spacejet) over a Mach number range of 1.50 to 2.86
- Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5
- Aerodynamics of bodies of revolution
- Aerodynamics of supersonic flight; : an introduction
- Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range
- Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds
- An Experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow
- An Investigation of the use of holography in studying supersonic flow in inlets.
- An accurate and rapid method for the design of supersonic nozzles
- An analysis of base pressure at supersonic velocities and comparison with experiment
- An analysis of buzzing in supersonic ram jets by a modified one-dimensional nonstationary wave theory
- An analysis of the instrumentation and operation of a supersonic wind tunnel
- An expansion of tables II and III of N.A.C.A. TN no. 1428
- An experimental investigation of a Mach 3.0 high-speed civil transport at supersonic speeds
- An initial experimental study of the effect of variations in frequency and impulse on the reduction in temperature recovery factor afforded by large-scale unsteady flow
- An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and a 40Â° sweepback : pressure distribution measurements of the interference effect of the wing on the fuselage at Mach numbers of 1.40 and 1.59
- Analysis and control of asymmetric vortex flows and supersonic vortex breakdown
- Analysis and control of asymmetric vortex flows and supersonic vortex breakdown : final report for the period December 1, 1991 to November 30, 1992
- Analysis and control of supersonic vortex breakdown flows
- Analysis and preliminary design of an optical instrument for the measurement of drop size and free-water content of clouds
- Analysis of an induction blowdown supersonic tunnel
- Analysis of flow dynamics through small diameter gas sampling systems
- Analytical investigation of fuel temperatures and fuel-evaporation losses encountered in long-range high-altitude supersonic flight
- Application of CFD to the analysis and design of high-speed inlets : final report
- Application of advanced computational codes in the design of an experiment for a supersonic throughflow fan rotor
- Application of oblique-shock sensing system to ram-jet-engine flight Mach number control
- Applications of Von Karman's integral method in supersonic wing theory
- Approximate solutions for the flow about flat-top wing-body configurations at high supersonic airspeeds
- Asymptotic theory of supersonic and viscous gas flows
- Automatic computation of wing-fuselage intersection lines and fillet inserts with fixed-area constraint
- Average skin-friction coefficients from boundary-layer measurements on an ogive-cylinder body in flight at supersonic speeds
- Axisymmetric supersonic flow in rotating impellers
- Body and canard effects on an attached-flow maneuver wing at Mach 1.62
- Bumblebee Program - aerodynamic data
- Calculation of aerodynamic heat transfer for blunt-nosed thin wings at different angles of attack at supersonic speeds
- Calculation of subsonic and supersonic steady and unsteady aerodynamic forces using velocity potential aerodynamic elements
- Calculation of surface temperatures in steady supersonic flight
- Calculation of three-dimensional, inviscid supersonic, steady flows
- Characteristics of a free supersonic helium jet issuing normally from a flat plate
- Characteristics of supersonic and hypersonic flow over blunt spiked bodies
- Collection and analysis of dynamic data with an instrumented aluminum high power rocket
- Combustion of aluminum borohydride in a supersonic wind tunnel
- Compilation and correlation of model starting loads from several supersonic wind tunnels
- Computation of separation ahead of blunt fin in supersonic turbulent flow
- Concorde aerodynamics and associated systems development
- Correlations of supersonic boundary-layer transition on cones including effects of large axial variations in wind-tunnel noise
- Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds
- Damping in roll of cruciform and some related delta wings at supersonic speeds
- Design and demonstration of a system for routine, boomless supersonic flights
- Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume II - code description
- Development of flow distortions in a full-scale nacelle inlet at mach numbers 0.63 and 1.6 to 2.0
- Development of supersonic computational aerodynamic program using panel method
- Development of the triplet singularity for the analysis of wings and bodies in supersonic flow
- Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine
- Effect of Reynolds number on the aerodynamic stability and control characteristics of a 55 degree clipped-delta-wing orbiter configuration at supersonic Mach numbers
- Effect of aspect ratio on undamped torsional oscillations of a thin rectangular wing in supersonic flow
- Effect of density gradients in confined supersonic shear layers
- Effect of leading-edge load constraints on the design and performance of supersonic wings
- Effect of planform and body on supersonic aerodynamics of multibody configurations
- Effect on tail-fin span on stability and control characteristics of a canard-controlled missile at supersonic Mach numbers
- Effects of forebody strakes and Mach number on overall aerodynamic characteristics on configuration with 55 cropped delta wing
- Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds
- Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55 ÌŠswept delta wing at supersonic speeds
- Effects of spanwise nozzle geometry and location on the longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds
- Elements of aerodynamics of supersonic flows
- Estimation of the static aerodynamic characteristics of ordnance projectiles at supersonic speeds
- Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds
- Euler flow predictions for an oscillating cascade using a high resolution wave-split scheme
- Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows
- Evaluation of five conical center-body supersonic diffusers at several angles of attack
- Experimental aerodynamic characteristics at Mach numbers from 0.60 to 2.70 of two supersonic cruise fighter configurations
- Experimental and computational study of a blunt cylinder-flare model in high supersonic flow
- Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
- Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements
- Experimental cavity pressure distributions at supersonic speeds
- Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
- Experimental effects of wing location on wing-body pressures at supersonic speeds
- Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities
- Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4
- Experimental investigation of leading-edge thrust at supersonic speeds
- Experimental investigation of porous-floor effects on cavity flow fields at supersonic speeds
- Experimental investigation of temperature recovery factors on bodies of revolution at supersonic speeds
- Experimental investigation to validate use of cryogenic temperatures to achieve high Reynolds numbers in boattail pressure testing
- Experimental pressure distributions over wing tips at Mach number 1.9, [Part] 2, Wing tip with subsonic trailing edge
- Extension of multigrid methodology to supersonic/hypersonic 3-D viscous flows
- Factors affecting the maximum lift-drag ratio at high supersonic speeds
- Factors affecting transition at supersonic speeds
- Final design of Sandia's supersonic parachute test vehicle
- Flight investigation at Mach numbers from 0.6 to 1.7 to determine drag and base pressures on a blunt-trailing-edge airfoil and drag of diamond and circular-arc airfoils at zero lift
- Flight test results of riblets at supersonic speeds
- Flow over a slender body of revolution at supersonic velocities
- Fluctuating loads measured on an over-the-wing supersonic jet model
- Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99, [Part] 2, Isentropic-spike all-external compression inlet
- Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
- Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
- Gas dynamics of thin bodies,
- Gasdynamics, theory and applications
- Heat transfer to blunt nose shapes with laminar boundary layers at high supersonic speeds
- Heat-transfer characteristics of blunt two-and three-dimensional bodies at supersonic speeds
- High speed aerodynamics and jet propulsion.
- High-speed aerodynamics : compressible flow.
- High-speed aerodynamics.
- High-speed computing machine calculation of supersonic axisymmetric flows
- Higher approximations in aerodynamic theory
- Improvement of accuracy of balanced-pressure indicators and development of an indicator calibrating machine
- In short, Episode 226, Thrust SSC
- Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds
- Inlet flowfield investigation, Part II., Computation of the flow about a supercruise forebody at supersonic speeds
- Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
- Interference effects of aft reaction-control yaw jets on the aerodynamic characteristics of a space shuttle orbiter model at supersonic speeds
- Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles
- Investigation at supersonic speeds of the compressor stall and inlet buzz characteristics of a J34 - spike-inlet combination
- Investigation at supersonic speeds of the variation with Reynolds number and Mach number of the total, base, and skin-friction drag of seven boattail bodies of revolution designed for minimum wave drag
- Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study, [Part] I, Design and experimental performance of standard turbine
- Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft
- Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds
- Investigation of flow characteristics over missile bodies at supersonic speeds
- Investigation of leading-edge flap performance on delta and double-delta wings at supersonic speeds
- Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord
- Investigation of the aerodynamic characteristics of the NACA RM-10 missile (with fins) at a Mach number of 1.62 in the Langley 9-inch supersonic tunnel
- Investigation of the drag of blunt-nosed bodies of revolution in free flight at Mach numbers from 0.6 to 2.3
- Investigation of the effects of model scale and stream Reynolds number on the aerodynamic characteristics of two rectangular wings at supersonic speeds on the Langley 9-inch supersonic tunnel
- Investigation of the variation with Reynolds number of the base, wave, and skin-friction drag of a parabolic body of revolution (NACA RM-10) at Mach numbers of 1.62, 1.93, and 2.41 in the Langley 9-inch supersonic tunnel
- Investigation of three types of supersonic diffuser over a range of Mach numbers from 1.75 to 2.74
- Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
- Investigations at supersonic speeds of the base pressure on bodies of revolution with and without sweptback stabilizing fins
- Lee-side flow over delta wings at supersonic speeds
- Line-vortex theory for calculation of supersonic downwash
- Loads on external stores at transonic and supersonic speeds
- Location of detached shock wave in front of a body moving at supersonic speeds
- Longitudinal aerodynamic characteristics of a model airplane configuration equipped with a scaled X-1 airplane wing
- Longitudinal aerodynamic characteristics of a vectored-engine-over-wing configuration at subsonic speeds
- Longitudinal and lateral-directional aerodynamic characteristics of a wing-cone configuration at Mach numbers from 2.5 to 4.5
- Low-speed aerodynamic characteristics of a highly swept, untwisted, uncambered arrow wing
- Measurement of recovery factors and friction coefficients for supersonic flow of air in a tube. : [Part] II, Results based on a two-dimensional flow model for entrance region
- Measurement of recovery factors and friction coefficients for supersonic flow of air in a tube. : [Part] II, Results based on a two-dimensional flow model for entrance region
- Mechanical property characterization of BorsicÂ®/aluminum laminates at room and elevated temperatures
- Methods for conducting short-time tensile, creep, and creep-rupture tests under conditions of rapid heating
- Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment
- New design concepts for high speed air transport
- Nonaxisymmetric viscous lower branch modes in axisymmetric supersonic flows
- Nonlinear conical flow
- Nonparallel instability of supersonic and hypersonic boundary layers
- Numerical analysis of supersonic flow through oscillating cascade sections by using a deforming grid
- Numerical simulation of steady supersonic viscous flow
- Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code
- Numerical simulations of supersonic flow through oscillating cascade sections
- Numerical solution in Lagrangian coordinates of a shock tube starting process
- On hypersonic blunt body flow fields obtained with a time-dependent technique
- PAN AIR, a computer program for predicting subsonic or supersonic linear potential flows about arbitrary configurations using a higher order panel method
- Performance of external-compression bump inlet at Mach numbers of 1.5 to 2.0
- Physics of heat exchange and gas dynamics.
- Planform effects on the supersonic aerodynamics of multibody configurations
- Prandtl-Meyer flow with sweep
- Prediction of vortex shedding from circular and noncircular bodies in supersonic flow
- Preliminary attempts at isothermal compression of a supersonic air stream
- Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62
- Pressure data for four analytically defined arrow wings in supersonic flow
- Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data
- Progress in supersonic cruise aircraft technology
- Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations
- Rolling and yawing moments for swept-back wings in sideslip at supersonic sppeds
- Screech noise source structure of a supersonic rectangular jet
- Secondary instability of high-speed flows and the influence of wall cooling and suction
- Semi-annual status report on NASA grant NSG 1629 "An investigation of vortex-induced aerodynamic characteristics of supersonic cruise configurations" : July 1, 1984 - December 31, 1984
- Shock capturing finite difference algorithms for supersonic flow past fighter and missile type configurations
- Slot jet interaction studies of an ogive cylinder at M[infinity] : 4 and 5
- Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3
- Some effects of fin plan form on the static stability of fin-body combinations at Mach number 4.06
- Some internal-flow characteristics at zero flight speed of an annular supersonic inlet and an open-nose inlet with sharp and rounded lips
- Some measurements at subsonic speeds of the aerodynamic forces and moments on two delta wings of aspect ratios 2 and 4 oscillating about the midchord
- Some observations on a new numerical method for solving the Navier-Stokes equations
- Some theoretical characteristics of trapezoidal wings in supersonic flow and a comparison of several wing-flap combinations
- Sonic limit singularities:, Part I:, General theory
- Sonic limit singularities:, Part II:, Examples
- Span loadings due to wing twist at transonic and supersonic speeds
- Spectral methods for modeling supersonic chemically reacting flow fields
- Stability derivatives of triangular wings at supersonic speeds
- Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4
- Statistical model of sonic boom structural damage
- Steady and nonsteady supersonic turbulent afterbody flow
- Study of lee-side flows over conically cambered delta wings at supersonic speeds
- Study of supersonic wings employing the attainable leading-edge thrust concept
- Supersonic aerodynamic characteristics of a proposed assured crew return capability (ACRC) lifting-body configuration
- Supersonic aerodynamic characteristics of a series of wrap-around-fin missile configurations
- Supersonic aerodynamic characteristics of a space shuttle orbiter model at angles of attack from 20 to 90
- Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration
- Supersonic aerodynamics and rocket propulsion,
- Supersonic aerodynamics of delta wings
- Supersonic aerodynamics, : a theoretical introduction
- Supersonic flow and shock waves
- Supersonic flow and shock waves
- Supersonic lift and pitching moment of thin sweptback tapered wings produced by constant vertical acceleration : Subsonic leading edges and supersonic trailing edges
- Supersonic magnus measurements of the 10-Caliber Army-Navy spinner projectile with wrap-around fins
- Supersonic nonlinear potential flow analysis : interim report
- Supersonic reacting internal flow fields
- Supersonic stability and control characteristics of a cruciform missile model with delta wings and aft tail fin controls
- Supersonic through-flow fan design
- Supersonic wings with significant leading-edge thrust at cruise
- Supersonic, nonlinear, attached-flow wing design for high lift with experimental validation
- Surface flow angles on an ogive cylinder at angle of attack in supersonic flow
- Surface pressure data for a supersonic-cruise airplane configuration at mach numbers of 2.30, 2.96, and 3.30
- Surface pressure data on a series of analytic forebodies at Mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip
- Surface pressure data on a series of conical forebodies at mach numbers from 1.70 to 4.50 and combined angles of attack and sideslip
- Survey and analysis of research on supersonic drag-due-to-lift minimumization with recommendations for wing design
- Systematic study of error sources in supersonic skin-friction balance measurements
- Tables of supersonic flow around cones of large yaw,
- Technology today, Episode 345
- Technology today, Episode 537
- The Calculation of downwash behind supersonic wings with an application to triangular plan forms
- The aerodynamic behavior of a harmonically oscillating finite sweptback wing in supersonic flow
- The aerodynamic design of the oblique flying wing supersonic transport
- The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow
- The natural flow wing-design concept
- The performance characteristics of a fixed geometry supersonic wind tunnel
- The potential theory of unsteady supersonic flow
- The proper combination of lift loadings for least drag on a supersonic wing
- The reversibility theorem for thin airfoils in subsonic and supersonic flow
- The static and dynamic longitudinal stability characteristics of some supersonic aircraft configurations
- The use of a laser doppler velocimeter in supersonic flow
- The use of perforated inlets for efficient supersonic diffusion
- The wedge hot-film anemometer in supersonic flow
- The yawing moment, due to sideslip of triangular, trapezoidal, and related plan forms in supersonic flow
- Theoretical and experimental engine-inlet flow fields for fighter forebodies
- Theoretical and experimental investigation of supersonic aerodynamic characteristics of a twin-fuselage concept
- Theoretical evaluation of high-speed aerodynamics for arrow-wing configurations
- Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds : Subsonic leading edges and trailing edges
- Theoretical loading at supersonic speeds of flat swept-back wings with interacting trailing and leading edges
- Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds
- Theoretical relations between the stability derivatives of a wing in direct and in reverse supersonic flow
- Theoretical study of air forces on an oscillating or steady thin wing in a supersonic main stream
- Theory of optimum aerodynamic shapes; : extremal problems in the aerodynamics of supersonic, hypersonic, and free-molecular flows
- Thermally perfect, calorically imperfect Taylor-Maccoll flow
- Three-degree-of-freedom evaluation of the longitudinal transfer functions of a supersonic canard missile configuration including changes in forward speed
- Transient aerodynamic behavior of an airfoil due to different arbitrary modes of nonstationary motions in a supersonic flow
- Translation A9-T. : advance copy
- Transonic and supersonic Euler computations of vortex-dominated flow fields about a generic fighter
- Turbulent boundary-layer temperature recovery factors in two-dimensional supersonic flow
- Turbulent shear layers in supersonic flow
- Turbulent shear layers in supersonic flow
- Unsteady flow in a supersonic cascade with two in-passage shocks
- Use of a characteristic surfaces for unsymmetrical supersonic flow problems
- User's guide to a system of finite-element supersonic panel flutter programs
- Velocity field of a round jet in a cross flow for various jet injection angles and velocity ratios
- Viscous flow simulations of internal store carriage and separation : final report for the period ended May 15, 1991
- Volterra's solution of the wave equation as applied to three-dimensional supersonic airfoil problems
- Wave-interactions in supersonic and hypersonic flows
- Wind-tunnel investigation at supersonic speeds of a canard-controlled missile with fixed and free-rolling tail fins
- Wind-tunnel investigation at supersonic speeds of a remote-controlled canard missile with a free-rolling-tail brake torque system
- Wind-tunnel investigation of the static lateral stability characteristics of wing-fuselage combinations at high supersonic speeds : Aspect-ratio series
- Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds
- Wind-tunnel/flight correlation study of aerodynamic characteristics of a large flexible supersonic cruise airplane (XB-70-1)
- Wing planform effects at supersonic speeds for an advanced fighter configuration
- Wing theory in supersonic flow,
- Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds

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