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

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

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- X-38 vehicle 131 flutter assessment
- A CFD/CSD interaction methodology for aircraft wings : a dissertation ...
- A Method for determining the aerodynamic characteristics of two- and three-dimensional shapes at hypersonic speeds
- A characteristic method for calculating the generalized flat flutter aerodynamic forces
- A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory
- A modification to linearized theory for prediction of pressure loadings on lifting surfaces at high supersonic Mach numbers and large angles of attack
- A modification to thin-airfoil-section theory, applicable to arbitrary airfoil sections, to account for the effects of thickness on the lift distribution
- A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing
- A new higher-order composite theory for analysis and design of high speed tilt-rotor blades
- A numerical model of unsteady, subsonic aeroelastic behavior
- A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M : 1.59 and angles of attack up to 36°
- A simplified method of elastic-stability analysis for thin cylindrical shells
- A study of facilities and fixtures for testing of a high speed civil transport wing component
- A study of means for rationalizing airplane design loads
- A summary of the forebody high-angle-of-attack aerodynamics research on the F-18 and the X-29A aircraft
- A survey of handling qualities criteria and their applications to high performance aircraft : final report
- A theory for lateral wing-tip blowing
- ASTROP2 users manual : a program for aeroelastic stability analysis of propfans
- Accuracy of approximate methods for predicting pressures on pointed nonlifting bodies of revolution in supersonic flow
- Active load control during rolling maneuvers
- Aerodynamic characteristics of a circular cylinder at Mach number 6.86 and angles of attack up to 90 degrees
- Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88
- Aerodynamic characteristics of a number of modified NACA four-digit-series airfoil sections
- Aerodynamic characteristics of a series of single-inlet air-breathing missile configurations
- Aerodynamic forces on freight trains
- 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 limitations of the UH-60A rotor
- Aerodynamic loading characteristics in sideslip of a 45° sweptback wing with and without a fence at high subsonic speeds
- Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section
- Aerodynamic properties of cruciform-wing and body combinations at subsonic, transonic, and supersonic speeds
- Aerodynamics of engine-airframe interaction : final report
- Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips
- Aircraft loading and structural layout
- Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
- Airfoil profiles for minimum pressure drag at supersonic velocities : application of shock-expansion theory, including consideration of hypersonic range
- An analysis of the pressure distribution measured on a body of revolution at transonic speeds in the slotted test section of the Langley 8-foot transonic tunnel
- An enhanced integrated aerodynamic load/dynamic optimization procedure for helicopter rotor blades
- An experimental and analytical method for approximate determination of the tilt rotor research aircraft rotor-wing download : final report, 05-30-94 - 11-30-85
- An experimental and theoretical analysis of the aerodynamic characteristics of a biplane-winglet configuration
- An experimental investigation of transonic flow past two-dimensional wedge and circular-arc sections using a Mach-Zehnder interferometer
- An experimental study of five annular air inlet configurations at subsonic and transonic speeds
- An experimental study of fluctuating pressure loads beneath swept shock/boundary layer interactions
- An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and a 40° sweepback : pressure distribution measurements of the interference effect of the wing on the fuselage at Mach numbers of 1.40 and 1.59
- An investigation of several NACA 1-series nose inlets with and without protruding central bodies at high-subsonic Mach numbers and at a Mach number of 1.2
- An investigation of tip planform influence on the aerodynamic load characteristics of a semi-span, unswept wing and wing-tip
- An investigation of tip planform influence on the aerodynamic load characteristics of a semi-span, unswept wing and wing-tip
- Analysis and compilation of missile aerodynamic data
- Analytical determination of the load on a trailing edge flap
- Analytical observations on the aerodynamics of a delta wing with leading edge flaps
- Application of a third order upwind scheme to viscous flow over clean and iced wings : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV
- Application of higher harmonic control to hingeless rotor systems
- CCBLADE documentation
- Calculation of flight vibration levels of the AH-1G helicopter and correlation with existing flight vibration measurements
- Calculation of the aerodynamic loading of flexible wings of arbitrary plan form and stiffness
- Center of pressure coefficients for airfoils at high speeds
- Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration
- Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings
- Chordwise and compressibility corrections to slender-wing theory
- Combined experiment : final report, Phase I
- Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade
- Comparison of concurrent strain gage- and pressure transducer-measured flight loads on a lifting reentry vehicle and correlation with wind tunnel predictions
- Comparison of wing-span averaging effects on lift, rolling moment, and bending moment for two span load distributions and for two turbulence representations
- Computational analysis of forebody tangential slot blowing on the high alpha research vehicle
- Computer programs for tethered-balloon system design and performance evaluation
- Control & reduction of unsteady pressure loads in separated shock wave turbulent boundary layer interaction : final report on NASA grant NAG 1-1471 for the period 01/09/93 through 01/01/95
- Correlation of forebody pressures and aircraft yawing moments on the X-29A aircraft at high angles of attack
- Design of a 4-1/2 stage turbine with a stage loading factor of 4.66 and high specific work output
- Determination of mean camber surfaces for wings having uniform chordwise loading and arbitrary spanwise loading in subsonic flow
- Determination of stores pointing error due to wing flexibility under flight load
- Development of an apparatus for wind tunnel dynamic experiments at high-α
- Development of an unsteady aerodynamic analysis for finite-deflection subsonic cascades
- Development of the triplet singularity for the analysis of wings and bodies in supersonic flow
- Divergence analysis report for the bodies of revolution model support systems
- Dynamics of the McDonnell Douglas large scale dynamic rig and dynamic calibration of the rotor balance
- Early operation experience on the ERDA/NASA 100 kW wind turbine
- Effect of an alternate winglet on the pressure and spanwise load distributions of a first-generation jet transport wing
- Effect of finite span on the airload distributions for oscillating wings
- Effect of propeller-axis angle of attack on thrust distribution over the propeller disk in relation to wake-survey measurement of thrust
- Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
- Effects of compressibility on maximum lift coefficients for six propeller airfoils
- Effects of flow separation and cove leakage on pressure and heat-transfer distributions along a wing-cove-elevon configuration at Mach 6.9
- Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
- Estimation of aircraft nonlinear unsteady parameters from wind tunnel data
- Experimental investigation of effects of blade tip geometry on loads and performance for an articulated rotor system
- Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading
- Experimental pressure distributions and force coefficients on block forms for varying Mach number, Reynolds number, and yaw angle
- Experimental pressure distributions over wing tips at Mach number 1.9, [Part] 2, Wing tip with subsonic trailing edge
- Experimental study of forces and moments on circular bodies at high angle of attack
- Experiments with fabrics for covering airplane wings, to determine effect of method of installation
- F-18 High Alpha Research Vehicle surface pressures : initial in-flight results and correlation with flow visualization and wind-tunnel data
- F-8 supercritical wing flight pressure, boundary-layer, and wake measurements and comparisons with wind tunnel data
- Final design proposal : the MANTA : an RPV designed to investigate forces and moments on a lifting surface
- Final technical report for aeroelastic analysis of counter rotation fans : NASA grant number NAG3-742; grant duration, September 1, 1986 to December 31, 1993
- Finite element thermo-viscoplastic analysis of aerospace structures
- 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
- Fluctuating loads measured on an over-the-wing supersonic jet model
- Flutter analysis of supersonic axial flow cascades using a high resolution euler solver, Part 1, Formulation and validation
- Full-scale hingeless rotor performance and loads
- Handbook of inviscid sphere-cone flow fields and pressure distributions
- Heat transfer and flow on the first stage blade tip of a power generation gas turbine, Part 1, Experimental results
- High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
- Higher harmonic control analysis for vibration reduction of helicopter rotor systems
- Implementation of a trailing-edge flap analysis model in the NASA Langley CAMRAD.MOD1/HIRES program
- Induced side forces on bodies of revolution at high angle of attack
- Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region
- Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45° sweptback highly tapered wing in combination with basic and indented bodies
- Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections
- Investigation of a technique for measuring dynamic ground effect in a subsonic wind tunnel
- Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
- Lift, pitching moment, and span load characteristics of wings at low speed as affected by variations of sweep and aspect ratio
- Lift-curve slopes determined in flight on a flexible swept-wing jet bomber
- Linearized lifting-surface theory for swept-back wings with slender plan forms
- Load distributions associated with controls at supersonic speeds
- Loads and Aeroelasticity Division research and technology accomplishments for FY 1987 and plans for FY 1988
- Loads associated with spoilers at supersonic speeds
- Loads on external stores at transonic and supersonic speeds
- Loads on wings due to spoilers at subsonic and transonic speeds
- Longitudinal stability characteristics at transonic speeds of a rocket-propelled model of an airplane having a 45 degree swept wing of aspect ratio 6.0
- Measurement and analysis of wing and tail buffeting loads on a fighter-type airplane
- Measurements of fluctuating pressures on the wing of a sweptback wind-body combination in the Langley 16-foot transonic tunnel
- Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds
- Modal forced vibration analysis of aerodynamically excited turbosystems : final report
- NASTRAN supplemental documentation for modal forced vibration analysis of aerodynamically excited turbosystems : final report
- Nacelle Aerodynamic and Inertial Loads (NAIL) project : summary report, Oct. 1979 - Aug. 1981
- Normal component of induced velocity in the vicinity of a lifting rotor with a nonuniform disk loading
- Note on the pressure distribution over the hull of elongated airships with circular cross section
- Numerical analysis of tangential slot blowing on a generic chined forebody
- On the distribution of lift along the span of an airfoil with displaced ailerons
- On the propagation of small perturbations in two simple aeroelastic systems
- Operational data reduction procedure for determining density and vertical structure of the Martian upper atmosphere from Mars global surveyor accelerometer measurements
- Parameter estimation of actuators for Benchmark Active Control Technology (BACT) wind tunnel model with analysis of wear and aerodynamic loading effects
- Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20
- Prediction of forces and moments for hypersonic flight vehicle control effectors : progress report and workplan
- Prediction of impact pressures, forces, and moments during vertical and oblique water entry
- Predictions of thermal buckling strengths of hypersonic aircraft sandwich panels using minimum potential energy and finite element methods
- Preliminary in-flight loads analysis of in-line launch vehicles using the VLOADS 1.4 program
- Preliminary results of supersonic-jet tests of simplified wing structures
- Pressure distribution and some effects of viscosity on slender inclined bodies of revolution
- Pressure distribution on the nose of an airship in circling flight
- Pressure distribution on wing ribs of the VE-7 and TS airplanes in flight
- Pressure distribution on wing ribs of the VE-7 and TS airplanes in flight. : Part 2: Pull-ups.
- Pressure distributions on sphere cones
- Pressure measurements on a body of revolution in the Langley 16-foot transonic tunnel and a comparison with free-fall data
- Refinements and tests of an advanced controller to mitigate fatigue loads in the Controls Advanced Research Turbine : preprint
- Remarks on the pressure distributions over the surface of an ellipsoid, moving translationally through a perfect fluid
- Report on the special field "interference" to the wind tunnel committee in February 1945
- Resume of air-load data on slats and flaps
- Rotorcraft dynamics 1984 : proceedings of the 2nd decennial Specialists' Meeting on Rotorcraft Dynamics sponsored by NASA Ames Research Center and the American Helicopter Society and held at NASA Ames Research Center, Moffett Field, California, November 7-9, 1984
- SOFIA II model telescope and wind tunnel test
- Self-compensating store ejection
- Sensitivity analysis for coupled aero-structural systems
- Simulation of iced wing aerodynamics
- Simultaneous optical measurements of axial and tangential steady-state blade deflections
- 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 measurements of aerodynamic forces and moments at subsonic speeds on a rectangular wing of aspect ratio 2 oscillating about the midchord
- Some notes on the aerodynamic loads associated with external-store installations
- Some properties of a five-parameter bivariate probability distribution
- Some tables of the factor of apparent additional mass
- Span loadings due to wing twist at transonic and supersonic speeds
- Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV
- Specimen designs for testing advanced aeropropulsion materials under in-plane biaxial loading
- Sphere-cone-cone surface pressure distribution at Mach numbers of 5, 6, 8, and 10
- Static multiple-load measurement technique as utilized in the Naval Surface Weapons Center's wind tunnels
- Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds
- Studies of air loads on man
- Summary of the modeling and test correlations of a NASTRAN finite element vibrations model for the AH-1G helicopter
- Surface pressure distributions on a large-scale 49° sweptback wing-body-tail configuration with blowing applied over the flaps and wing leading edge
- System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality : a dissertation ...
- Test of NACA 66,2-116, a : 0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane
- Tests of four models representing intermediate sections of the XB-33 airplane including sections with slotted flap and ailerons
- The accuracy of parameter estimation in system identification of noisy aircraft load measurement
- The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds
- The local motions of a payload supported by a tritethered natural shape balloon
- The proper combination of lift loadings for least drag on a supersonic wing
- Theoretical and experimental study of twisted and cambered delta wings designed for a Mach number of 3.5
- Theoretical antisymmetric span loading for wings of arbitrary plan form at subsonic speeds
- Theoretical loading at supersonic speeds of flat swept-back wings with interacting trailing and leading edges
- Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds
- Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow
- Thermal stress analysis of ceramic gas-path seal components for aircraft turbines
- Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
- Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6
- Turbine blade-tip clearance excitation forces : final report on Contract number NAS8-35018
- Two projectiles connected by a flexible tether dropped in the atmosphere
- Two-component force balance for measuring skin friction and side force
- Variation of peak pitching-moment coefficients for six airfoils as affected by compressibility
- Wind-tunnel investigation of aerodynamic loading on a 0.237-scale model of a remotely piloted research vehicle with a thick, high-aspect-ratio supercritical wing
- Wind-tunnel investigation of the effects of steady rolling on the aerodynamic loading characteristics of a 45° sweptback wing at high subsonic speeds
- Wind-tunnel measurements of air loads on split flaps

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