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Airplanes -- Wings, Triangular
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The concept ** Airplanes -- Wings, Triangular** represents the subject, aboutness, idea or notion of resources found in **University of Oklahoma Libraries**.

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Airplanes -- Wings, Triangular
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**Airplanes -- Wings, Triangular**represents the subject, aboutness, idea or notion of resources found in**University of Oklahoma Libraries**.- Label
- Airplanes -- Wings, Triangular

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- [Numerical computation of viscous flow around bodies and wings moving at supersonic speeds] : final report, NASA grant NGR 16-002-003, November 15, 1971 - March 31, 1984
- A note on the drag due to lift of delta wings at Mach numbers up to 2.0
- A preliminary wind-tunnel investigation of flutter characteristics of delta wings
- A study of the vortex flow over 76/40-deg double-delta wing
- A theory for lateral wing-tip blowing
- Advanced hypersonic aircraft design
- Aerodynamic characteristics at Mach 6 of a hypersonic research airplane concept having a 70 ̊swept delta wing
- Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section : Transonic-bump method
- Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04
- Aerodynamic characteristics over a Mach number range of 1.40 to 2.78 of a rocket-propelled airplane configuration having a low 52.2° delta wing and an unswept horizontal tail
- Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow
- An aerodynamic model for one and two degree of freedom wing rock of slender delta wings
- An analytical design procedure for the determination of effective leading edge extensions on thick delta wings
- An exploratory study of apex fence flaps on a 74-degree delta wing
- Analytical observations on the aerodynamics of a delta wing with leading edge flaps
- Analytical studies of separated vortex flow on highly swept wings
- Breaking down the delta wing vortex : the role of vorticity in the breakdown
- Comparison of lift-curve slopes for a model tested in two slotted tunnels of different sizes at high subsonic speeds
- Configuration heating for a hypersonic research airplane concept having a 70 ̊swept double-delta wing
- Conical Euler analysis and active roll suppression for unsteady vortical flows about rolling delta wings
- Conical Euler simulation and active suppression of delta wing rocking motion
- Control hinge-movement and effectiveness characteristics of several interchangeable tip controls on a 60° delta wing at Mach numbers of 1.41, 1.62, and 1.96
- Damping in roll of cruciform and some related delta wings at supersonic speeds
- Damping in roll of models with 45°, 60°, and 70° delta wings determined at high subsonic, transonic, and supersonic speeds with rocket -powered models
- Design and construction of a remote piloted flying wing
- Development of aerodynamic prediction methods for irregular planform wings
- Dual methods and approximation concepts in structural synthesis
- Dual methods and approximation concepts in structural synthesis
- Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing
- 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 leading- and trailing-edge flaps on clipped delta wings with and without wing camber at supersonic speeds
- Effect of some section modifications and protuberances on the zero-lift drag of delta wings at transonic and supersonic speeds
- Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60° delta wing at Mach numbers from 0.75 to 1.96
- 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 size of external stores on the aerodynamic characteristics of an unswept and a 45° sweptback wing of aspect ratio 4 and a 60° delta wing at Mach numbers of 1.41, 1.62, and 1.96
- Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds
- Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model
- Effects of wing position and vertical-tail configuration on stability and control characteristics of a jet-powered delta-wing vertically rising airplane model
- Evaluation of Navier-Stokes and Euler solutions for leading-edge separation vortices
- Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
- Experimental and theoretical study of three interacting, closely-spaced, sharp-edged 60?delta wings at low speeds
- Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
- Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60° delta-wing airplane model
- Experimental results of the control of a vortical flow by tangential blowing
- Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations
- Flow field over the wing of a delta-wing fighter model with vortex control devices at Mach 0.6 to 1.2
- Flow past a flat plate with a vortex/sink combination
- Flutter of a 60° delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model
- Force and moment measurements on a 74 ̊delta wing with an apex flap (data report)
- High-alpha vortex decoupling investigations on a chine forebody/delta wing configuration at transonic mach numbers
- Influence of airfoil geometry on delta wing leading-edge vortices and vortex-induced aerodynamics at supersonic speeds
- Investigation of the "vortex tab"
- 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
- Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
- Lee-side flow over delta wings at supersonic speeds
- Lift and moment on oscillating triangular and related wings with supersonic edges
- Lift augmentation on a delta wing via leading edge fences and the Gurney flap
- Low-speed pitching derivatives of low-aspect-ratio wings of triangular and modified triangular plan forms
- Low-speed static lateral stability characteristics of a canard model having a 60° triangular wing and horizontal tail
- Low-speed static stability characteristics of a cambered-delta-wing model
- Navier-Stokes and Euler solutions for lee-side flows over supersonic delta wings : a correlation with experiment
- Numerical solutions of Navier-Stokes equations for a Butler wing
- Numerical solutions of Navier-Stokes equations for a Butler wing : progress report for the period ending August 31, 1985
- Numerical study of delta wing leading edge blowing
- On the range of applicability of the transonic area rule
- On the range of applicability of the transonic area rule
- Preliminary investigation at supersonic speeds of triangular and sweptback wings
- Research in computational fluid dynamics : semiannual progress report, reporting period September 1, 1986 - February, 1987
- Some low-speed flutter characteristics of simple low-aspect-ration delta wing models
- 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
- Stability derivatives of triangular wings at supersonic speeds
- Stability of streamwise vortices : progress report for the period ended April 1, 1986
- Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
- Subsonic aerodynamic characteristics of a circular body earth-to-orbit vehicle
- Subsonic investigations of vortex interaction control for enhanced high-alpha aerodynamics of a chine forebody/delta wing configuration
- Supersonic aerodynamics of delta wings
- Supersonic flutter of a 60° delta wing encountered during the flight test of a rocket-propelled model
- The Calculation of downwash behind supersonic wings with an application to triangular plan forms
- The Delta monster : an RPV designed to investigate the aerodynamics of a delta wing platform : final design proposal
- The art of sharp-leading-edged delta wings with blowing
- The effects of fuselage size on the low-speed longitudinal aerodynamic characteristics of a thin 60° delta wing with and without a double slotted flap
- The lateral-directional characteristics of a 74-degree delta wing employing gothic planform vortex flaps
- Theoretical and experimental investigation of vortex breakdown : final technical report, June 1, 1985 - May 31, 1986
- Theoretical studies on flapped delta wings
- Three-dimensional unsteady lift problems in high-speed flight : the triangular wing
- Transonic Navier-Stokes calculations about a 65−p0−s delta wing
- Transonic flutter investigation of two 50° semispan modified-delta wings with tip ailerons
- Wind tunnel investigation of the interaction and breakdown characteristics of slender-wing vortices at subsonic, transonic, and supersonic speeds
- Wind-tunnel investigation at high subsonic speeds to determine the rolling derivatives of two wing-fuselage combinations having triangular winds, including a semiempirical method of estimating the rolling derivatives
- Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack
- Wind-tunnel investigation of the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4

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