Computation of Shock-Free Transonic Flows for Airfoil Design (Classic Reprint)

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Excerpt from Computation of Shock-Free Transonic Flows for Airfoil Design

Steady shock-free transonic compressible fluid flow about a series of symmetric airfoils without circulation is found by computing analytic solutions of the hodograph equations for an ideal polytropic gas in two dimensions.

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Details

Publisher - Forgotten Books

Author(s) - David G. Korn

Hardback

Published Date -

ISBN - 9780331357370

Dimensions - 22.9 x 15.2 x 0.9 cm

Page Count - 109

Paperback

Published Date -

ISBN - 9781332115433

Dimensions -

Page Count -

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