Viscous effects on the flow coefficient for a supersonic nozzle
- 1 March 1970
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 8 (3) , 605-607
- https://doi.org/10.2514/3.5728
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Laminarization of a turbulent boundary layer in nozzle flow.AIAA Journal, 1969
- Far-wake behavior of hypersonic blunted cones.AIAA Journal, 1967
- A review of microrocket technology - 10 super minus 6 to 1 lbf thrust.Journal of Spacecraft and Rockets, 1966
- Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic regionAIAA Journal, 1965
- GROWTH OF THE TURBULENT WAKE BEHIND A SUPERSONIC SPHEREAIAA Journal, 1963
- Turbulent Diffusion in the Wake of a Blunt-Nosed Body at Hypersonic SpeedsJournal of the Aerospace Sciences, 1962
- Width of the Turbulent Trail behind a Hypervelocity SpherePhysics of Fluids, 1961