Sidewall boundary-layer effects in two-dimensional airfoil testing progress report for the period ending June 1985 /

Sidewall boundary-layer effects in two-dimensional airfoil testing progress report for the period ending June 1985 /

"Theoretical studies required to evaluate and validate the streamlined wall test section of the 0.3 m transonic Cryogenic Tunnel were initiated. The various aspects that are being considered presently are deviations of the real wall shape from the true streamline shape, wall adjustment strategy...

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Bibliographic Details
Main Author: Murthy, A. V
Corporate Authors: Langley Research Center, Old Dominion University Department of Mechanical Engineering and Mechanics
Other Authors: Goglia, G. L
Format: Government Document Book
Language:English
Published: Norfolk, Va. : Dept. of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University, [1985]
Series:NASA contractor report NASA CR-176034
Subjects:
Aerofoils > Testing
Laminar boundary layer > Testing
Transonic wind tunnels > Computer simulation
Airfoils
Boundary layers
Cryogenic wind tunnels
Laminar flow
Transonic wind tunnels
Wall pressure
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Stanford University

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Call Number: ISIL:US-CST
NAS 1.26:176034

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