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Cover image for Wind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration

Wind tunnel investigation of the supersonic stage separation aerodynamics of a generic 0.0175- scale bimese two-stage-to-orbit reusable launch vehicle configuration

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Cover image for Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed

Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed

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Cover image for Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique

Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique

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Cover image for Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds

Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds

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Cover image for Analysis of a split-plot experimental design applied to a low-speed wind tunnel investigation

Analysis of a split-plot experimental design applied to a low-speed wind tunnel investigation

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Cover image for Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields

Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields

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Cover image for Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods

Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods

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Cover image for Fiber-optic-based laser vapor screen flow visualization sysytem for aerodynamic research in larger scale subsonic and transonic wind tunnels

Fiber-optic-based laser vapor screen flow visualization sysytem for aerodynamic research in larger scale subsonic and transonic wind tunnels

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Joyner - Microforms B300 NAS 1.15:4514 ✔ Available