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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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Performance characteristics of underslung vertical wedge inlet with porous suction at Mach numbers of 0.63 and 1.5 to 2.0
Admittance of wedge excited coaxial antenna with plasma sheath
Aperture reflection coefficient of parallel plate waveguide by wedge diffraction analysis
Spectrometers, utilizing interference filter wedges, for field use, especially in hostile environments
Design criteria for Nimbus D infrared filter wedge spectrometer
Real gas wedge-induced laminar separation on cooled blunt flat plate at hypersonic speed
Effect of boundary layer bleed on heat transfer and pressure distributions over wedge-flap surface at hypersonic speeds
Aerodynamic characteristics of two blunt half cone wedge entry configurations at supersonic speeds
Supersonic wind tunnel investigation of aerodynamic force characteristics of jet issuing transverse to wedge model
Reflectance of wedge angle parallel plate waveguides in transverse electromagnetic mode illuminating reflecting sheet
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer separation at moderate enthalpies in hypersonic flow
Ion current drawn to conducting wedge in collisionless plasma flow, deducing flow velocity and ion number density
Doppler shift measurements with double wedge technique applied to mass motion of air plasma escaping ends of theta pinch
Hypersonic flow over blunted slender wedges, examining contradiction between Chernyi and Cheng integral methods for oscillator behavior of shock shape and pressure
Heat transfer and pressure distributions inside hinge line gap of wedge-flap combination at hypersonic speeds
Wedge induced laminar boundary layer separation on flat plate in low density
Analytic formulation of three wedge angle constraints in trajectory studies
Surface pressures and shock wave shapes on sharp flat plates and wedges in rarefied hypersonic transition flow with emphasis on merged layer regime