Flow coefficients for supersonic nozzles with comparatively small radius of curvature throats
- 1 February 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (2) , 196-198
- https://doi.org/10.2514/3.30247
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Viscous effects on the flow coefficient for a supersonic nozzleAIAA Journal, 1970
- Transonic flow in small throat radius of curvature nozzles.AIAA Journal, 1969
- Transonic flowfield in a supersonic nozzle with small throat radius of curvature.AIAA Journal, 1969
- Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic regionAIAA Journal, 1965
- The compressible flow discharge coefficients for a two-dimensional slitInternational Journal of Mechanical Sciences, 1965
- TRANSONIC FLOW IN TWO-DIMENSIONAL AND AXIALLY-SYMMETRIC NOZZLESThe Quarterly Journal of Mechanics and Applied Mathematics, 1962
- On the Flow of a Compressible Fluid through OrificesProceedings of the Institution of Mechanical Engineers, 1955