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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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Longitudinal aerodynamic characteristics of delta wings with curved & straight leading edges from mach 3 to 6
Delta modulation as a pulse duration-amplitude modulation system, using transform methods and digital computation
Wind tunnel tests on aspect ratio 2.17 delta wing model with midchord boundary layer control flaps
Pressure measurements in flight over conically cambered delta wing of F-102A aircraft at transonic speeds
High subsonic speed of static longitudinal aerodynamic characteristics of delta wing configuration for angle of attack from 0 deg to 90 deg
Aerodynamic loads on external store adjacent to 60 deg delta wing at Mach numbers 0.75 to 1.96
Free flight drag measurements on delta wing with wing-fuselage-store
Wing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Mach 2.01
Adsorption phenomena in noble metals rhodium, iridium, palladium, and gold - application of potentiostatic delta method
Pressure and heat transfer over 80-degree sweep slab delta wing in hypersonic flow - wind tunnel test
Maximum lift-drag ratios of delta wing half-cone combinations in hypersonic helium wind tunnel to determine interference lift
Performance test data for pressure distributions over 60 deg delta wing at Mach 1.61 and 2.01
Wing sweep and blunting effects on delta planforms in helium flow at Mach 20
Lift-drag-ratio characteristics of rectangular and delta wings at Mach 6.9
Investigation of half-cone delta wing configurations under laminar boundary layer conditions at Mach 6.86 to determine favorable interference effects on maximum lift-drag ratio
Wing-tip droop effects on performance and stability of canard delta-wing aircraft at supersonic speeds
Wind tunnel testing of two and four engine models of delta wing aircraft for transonic drag rise increment and maximum lift-drag ratio comparison
Wind tunnel investigation of delta-wing-body combination sonic boom at Mach 1.41 and 2.01