Influence of initial flow direction on the turbulent base pressure in supersonic axisymmetric flow
- 1 December 1970
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 7 (12) , 1484-1488
- https://doi.org/10.2514/3.30202
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Determination of the turbulent base pressure in supersonic axisymmetric flow.Journal of Spacecraft and Rockets, 1968
- Turbulent separation associated with axisymmetric flared bodies.Journal of Spacecraft and Rockets, 1967
- Turbulent boundary-layer separation in front of a forward-facing step.AIAA Journal, 1967
- 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
- THE EFFECTS OF BASE BLEED AND SUSTAINER ROCKET NOZZLE DIAMETER AND LOCATION ON THE BASE DRAG OF A BODY OF REVOLUTION WITH CONCENTRIC BOOST AND SUSTAINER ROCKET NOZZLESPublished by Defense Technical Information Center (DTIC) ,1963