Aerodynamic Performance and Pressure Distributions for a NASA SC(2)-0714 Airfoil Tested in the Langley 0.3-meter Transonic Cryogenic Tunnel PDF Download

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Aerodynamic Performance and Pressure Distributions for a NASA SC(2)-0714 Airfoil Tested in the Langley 0.3-meter Transonic Cryogenic Tunnel

Aerodynamic Performance and Pressure Distributions for a NASA SC(2)-0714 Airfoil Tested in the Langley 0.3-meter Transonic Cryogenic Tunnel PDF Author: Renaldo V. Jenkins
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 308

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