Transonic flowfield in a supersonic nozzle with small throat radius of curvature.
- 1 July 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (7) , 1364-1366
- https://doi.org/10.2514/3.5349
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Transonic flow in small throat radius of curvature nozzles.AIAA Journal, 1969
- Flow phenomena and convective heat transfer in a conical supersonic nozzle.Journal of Spacecraft and Rockets, 1967
- Detection of oblique shocks in a conical nozzle with a circular-arc throat.AIAA Journal, 1966
- Effect of small radius of curvature on transonic flow in axisymmetric nozzles.AIAA Journal, 1966
- A suggestion for the numerical solution of the steady Navier-Stokes equations.AIAA Journal, 1965
- Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic regionAIAA Journal, 1965
- TRANSONIC FLOW IN TWO-DIMENSIONAL AND AXIALLY-SYMMETRIC NOZZLESThe Quarterly Journal of Mechanics and Applied Mathematics, 1962