Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds /

Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds /

Theoretical pressure distributions on nonlifting circular-arc airfoils in two-dimensional flows with high subsonic free-stream velocity are found by determining approximate solutions, through an iteration process, of an integral equation for transonic flow proposed by Oswatitsch. The integral equati...

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Bibliographic Details
Main Author: Spreiter, John R
Corporate Author: United States National Advisory Committee for Aeronautics
Other Authors: Alksne, Alberta Y
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1954
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3096
Subjects:
Aerodynamic load
Aerofoils
Integral equations
Iterative methods (Mathematics)

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Stanford University

Holdings details from Stanford University
Call Number: ISIL:US-CST
NACA TN 3096

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