Flow phenomena and convective heat transfer in a conical supersonic nozzle.
- 1 August 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 4 (8), 1040-1047
- https://doi.org/10.2514/3.29015
Abstract
No abstract availableThis publication has 18 references indexed in Scilit:
- Detection of oblique shocks in a conical nozzle with a circular-arc throat.AIAA Journal, 1966
- Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic regionAIAA Journal, 1965
- Shock predictions in conical nozzlesAIAA Journal, 1965
- Turbulent Boundary-Layer Heat Transfer from Rapidly Accelerating Flow of Rocket Combustion Gases and of Heated AirPublished by Elsevier BV ,1965
- The viscosity of dry and humid airInternational Journal of Heat and Mass Transfer, 1964
- Convective heat transfer in a convergent-divergent nozzleInternational Journal of Heat and Mass Transfer, 1964
- SHOCK FORMATION IN CONICAL NOZZLESAIAA Journal, 1963
- EXPERIMENTAL INVESTIGATION OF HEAT TRANSFER RATES IN ROCKET THRUST CHAMBERSAIAA Journal, 1963
- Characteristics of Conical Supersonic NozzlesARS Journal, 1962
- Heat Transfer to Separated and Reattached Subsonic Turbulent Flows Obtained Downstream of a Surface StepJournal of the Aerospace Sciences, 1959