Boundary-layer analysis of low-density nozzles, including displacement, slip, and transverse curvature

Publisher Website

1 April 1970

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

Vol. 7 (4) , 462-468
https://doi.org/10.2514/3.29964

Abstract

No abstract available

Keywords

This publication has 5 references indexed in Scilit:

Binary boundary layers on sharp cones in low-density supersonic and hypersonic flow.
AIAA Journal, 1969
Design of axisymmetric contoured nozzles for laminar hypersonic flow.
Journal of Spacecraft and Rockets, 1968
Convective heating in regions of large favorable pressure gradient.
AIAA Journal, 1967
Solution to the binary diffusion laminar boundary-layer equations with second-order transverse curvature.
AIAA Journal, 1967
Local heat-transfer coefficients in a nozzle with high-speed laminarflow.
AIAA Journal, 1965