Investigation of the Effect of the Fuselage on the Wing of a Low-Wing Monoplane
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FUSELAGES, RECTANGULAR↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Effects of wing incidence on the longitudinal trim characteristics of a cambered 70 deg delta-wing configuration at mach numbers 3.0 to 5.0
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INCIDENCE↗
Effects of wing position and fuselage size on the low-speed static and rolling stability characteristics of a delta-wing model
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STABILITY, LATERAL - STATIC↗
LOW DENSITY, AUTOROTATING WINGS FOR MANNED REENTRY. I - CONCEPTS OF ROTARY WING ATMOSPHERIC ENTRY
Aerodynamic and structural aspects of rotary atmospheric entry aids, including high temperature rotor material selection, rotor blade design and drag and lift modulation problems
ATMOSPHERIC ENTRY↗
Effectiveness of Warm-Start PPO for Guidance with Highly Constrained Nonlinear Fixed-Wing Dynamics
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Coletti, Christian↗
Wing selection as influenced by the effect of wing bending on aerodynamic-center shift
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Mathews, C. W.↗
Aerodynamic characteristics in pitch at a Mach number of 1.97 of two variable-wing- sweep V/STOL configurations with outboard wing panels swept back 75 deg
Aerodynamic characteristics in pitch of variable sweep V/STOL configurations tested in supersonic wind tunnel
AERODYNAMIC CHARACTERISTICS↗
Wing pressure distributions over the lift range of the convair xf-92a delta-wing airplane at subsonic and transonic speeds
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Jordan, G. H.↗
A wind tunnel investigation to evaluate the aerodynamic performance of three different airplane configurations having arrow-wing and delta-wing plan forms at a Mach number of 2.91
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Grimaud, J. E.↗
Idealized Wings and Wing-Bodies at a Mach Number of 3
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Elliot D Katzen↗
Space shuttle: Static stability and control investigation of NR/GD delta wing booster (B-20) and delta wing orbiter (134D), volume 4
Test results of booster and orbiter models of various component buildup configurations are reported. Dataset Collation Sheets, which give a complete summary of the configurations, are presented along with a description of the test facility. Data reduction procedures are described.
Allen, E. C., Jr.↗
Large-scale wind-tunnel tests of an airplane model with a 45 deg sweptback wing of aspect ratio 2.8 with area suction applied to trailing-edge flaps and with several wing leading-edge modifications
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Koenig, D. G.↗
Aerodynamics of bodies, wings, and wing-body combinations at high angles of attack and supersonic speeds
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Nielsen, J. N.↗
Aerodynamic-center considerations of wings and wing-body combinations
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Lamar, J. E.↗
An integrated approach to the analysis and design of wings and wing-body combinations in supersonic flow
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Carmichael, R. L.↗
Some methods for reducing wing drag and wing-Nacelle interference
Primary efforts directed toward drag reduction centered on the design of both supercritical and subcritical families of airfoils, the reduction of induced drag through the use of vortex diffusers, and the reduction of interference drag for executive-type aircraft.
Kelly, T. C.↗