Wind-tunnel simulation of rocket vehicles in flight with two-phase-flow rocket plumes.

Publisher Website

1 April 1967

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

Vol. 4 (4) , 518-524
https://doi.org/10.2514/3.28897

Abstract

No abstract available

Keywords

This publication has 4 references indexed in Scilit:

VISUALIZATION OF FLOW PATTERNS ON WIND TUNNEL MODELS BY MEANS OF OIL FLOW AND THERMAL PAINT TECHNIQUES
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1964
Nozzle contours for minimum particle-lag loss
AIAA Journal, 1963
Recent Advances in Gas-Particle Nozzle Flows
ARS Journal, 1962
Light Scattering by Small Particles
Physics Today, 1957