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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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Supersonic store interference - 1, swept-wing heavy bomber with large stores - lift & drag at mach 1.61
Free flight tests of 45-deg swept wings of 3.15 aspect ratio and 0.54 taper ratio to measure wing damping and possible transonic flutter
Effect of large store /nacelle/ on a swept-wing heavy bomber - lateral force and pitching moments
Origin of supersonic store interference from measurements of individual forces - swept-wing fighter-bomber with large & small stores
Aerodynamic load and flutter on swept and unswept wings at various speeds
Factors affecting flutter characteristics calculated for two swept wings
Aerodynamic characteristics of aircraft configurations with highly swept twisted and cambered arrow wings at hypersonic speeds
Stall characteristics of swept wing configurations
Stability and control of variable sweep wing configuration with outboard wing panels swept back 75 degrees at Mach 2.01
Forces and moments of store-pylon combination mounting on swept wing-fuselage configuration in supersonic pressure tunnel
Static force and interference drag on externally carried bomb in flow field of supersonic, swept wing fighter-bomber aircraft
Longitudinal and lateral stability and control characteristics of swept wing fighter aircraft
Wind tunnel investigations of effect on static stability of modifications to swept wing fighter aircraft model
Lateral-directional augmentation to improve handling qualities of swept wing jet transport operating at STOL air speeds
Pressure distributions on flat plate delta wing swept 65 deg at hypersonic speeds at angles of attack from 65 deg to 115 deg and angles of roll from 0 deg to 25 deg at 90 deg angle of attack
Swept wing fighter aircraft drag coefficient reduction by configuration redesign
Free flight tunnel testing of swept wing aircraft model to determine roll effectiveness of differentially deflected horizontal tail