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Renaldo V Jenkins
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NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
Renaldo V. Jenkins · Langley Research Center
55 sayfa · 1989
Aerofoils / Supercritical airfoils / Wind tunnel walls
Reynolds number tests of an NPL 9510 airfoil in the Langley 0.3-meter transonic cryogenic tunnel
Renaldo V Jenkins · For sale by the National Technical Information Service]
84 sayfa · 1983
Reynolds number / Testing / Aerofoils
Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter Transonic Cryogenic Tunnel
Renaldo V. Jenkins · For sale by the National Technical Information Service]
Sayfa sayısı yok · 1988
Reynolds number / Testing / Aerofoils
Tables for correcting airfoil data obtained in the Langley 0.3-meter transonic cryogenic tunnel for sidewall boundary layer effects
Renaldo V. Jenkins · National Aeronautics and Space Administration, Langley Research Center
Sayfa sayısı yok · 1986
Transonic wind tunnels / Aerofoils
R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
Renaldo V. Jenkins · For sale by the National Technical Information Service
Sayfa sayısı yok · 1986
Transonic wind tunnels / Statistics / Wall pressure (Aerodynamics) / Reynolds number / Testing