Supersonic nozzle discharge coefficients at low Reynolds numbers
- 1 September 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (9) , 1876-1879
- https://doi.org/10.2514/3.6443
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Some numerical results on viscous low-density nozzle flows in the slender-channel approximationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic regionAIAA Journal, 1965
- Turbulent Boundary-Layer Heat Transfer from Rapidly Accelerating Flow of Rocket Combustion Gases and of Heated AirPublished by Elsevier ,1965
- Nozzle characteristics in the transition regime between continuum and free molecular flowAIAA Journal, 1964
- A Semiempirical Description of the Discharge Characteristics of the Converging Section of a Low-Density Hypersonic NozzleJournal of the Aerospace Sciences, 1961