Rotational axisymmetric mean flow and damping of acoustic waves in asolid propellant rocket.
- 1 August 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 4 (8) , 1462-1464
- https://doi.org/10.2514/3.3709
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Shock tube test time limitation due to turbulentwall boundary layerAIAA Journal, 1964
- Test Time in Low-Pressure Shock TubesPhysics of Fluids, 1963
- Effect of Boundary-Layer Growth in a Shock Tube on Shock Reflection from a Closed EndPhysics of Fluids, 1961
- The Tailored-Interface Hypersonic Shock TunnelJournal of the Aerospace Sciences, 1959