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December 10, 2009 | History

A novel technique for controlling shock strength of laminar-flow aerofoil sections 1 edition

A novel technique for controlling shock strength of laminar-flow aerof ...
P. R. Ashill

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A novel technique for controlling shock strength of laminar-flow aerofoil sections
by P.R. Ashill, J.L. Fulker, A. Shires.

Published 1993 by Defence Research Agency in Farnborough .
Written in English.

Edition Notes

Series
Technical memorandum aerodynamics and propulsion -- 13

ID Numbers

Open Library
OL17234087M

History Created December 10, 2009 · 1 revision Download catalog record: RDF / JSON

December 10, 2009 Created by WorkBot add works page