Laminar boundary-layer development on yawed cone

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1 April 1964

journal article
research article
Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal

Vol. 2 (4) , 775-776
https://doi.org/10.2514/3.2410

Abstract

No abstract available

This publication has 1 reference indexed in Scilit:

AN INTEGRAL METHOD FOR CALCULATION OF SUPERSONIC LAMINAR BOUNDARY LAYER WITH HEAT TRANSFER ON YAWED CONE
AIAA Journal, 1963