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United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
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1
Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter Transonic Cryogenic Tunnel /
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Jenkins, Renaldo V.
Published 1988
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Effects of independent variation of Mach and Reynolds numbers on the low-speed aerodynamic characteristics of the NACA 0012 airfoil section /
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Ladson, Charles L.
Published 1988
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Turbulent flow in a 180 ̊bend : modeling and computations /
by
Kaul, Upender K.
Published 1989
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Flight Mechanics/Estimation Theory Symposium, 1989 : proceedings of a symposium sponsored by NASA Goddard Space Flight Center and held at Goddard Space Flight Center, Greenbelt, Ma...
Published 1989
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Hot-jet simulation in cryogenic wind tunnels.
by
Asai, Keisuke
Published 1989
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United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Asai, Keisuke
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Flight Mechanics/Estimation Theory Symposium Goddard Space Flight Center
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Hill, Acquilla S.
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Jenkins, Renaldo V.
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Kaul, Upender K.
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Ladson, Charles L.
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Ray, Edward J.
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Stengle, Thomas
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