Determination of the turbulent base pressure in supersonic axisymmetric flow.
- 1 January 1968
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (1) , 101-107
- https://doi.org/10.2514/3.29192
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Experimental studies on the lip shockPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1967
- The effect of initial conditions on the development of a free shear layerJournal of Fluid Mechanics, 1966
- The Turbulent Supersonic Base Pressure Problem: A Comparison between a Theory and Some Experimental EvidenceAeronautical Quarterly, 1966
- A review of hypersonic wake studies.AIAA Journal, 1966
- Comments on "Review of Recent Developments in Turbulent Supersonic Base Flow"AIAA Journal, 1966
- An Analysis of the Turbulent Base Pressure Problem in Supersonic Axisymmetric FlowAeronautical Quarterly, 1965
- TRANSIENT BASE PRESSURE STUDY OF AN AXISYMMETRIC SUPERSONIC MISSILE FLYING HEAD-ON THROUGH A BLAST WAVEPublished by Office of Scientific and Technical Information (OSTI) ,1964
- COMPRESSIBLE JET SPREAD PARAMETER FOR MIXING ZONE ANALYSESAIAA Journal, 1963
- An Experimental Investigation of Base Flows at Supersonic SpeedsJournal of the Royal Aeronautical Society, 1961