Comparison of measured and predicted flows through conical supersonic nozzles, with emphasis on the transonic region
- 1 September 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 3 (9) , 1606-1614
- https://doi.org/10.2514/3.3216
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Convective heat transfer in a convergent-divergent nozzleInternational Journal of Heat and Mass Transfer, 1964
- SHOCK FORMATION IN CONICAL NOZZLESAIAA Journal, 1963
- SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVER-EXPANDED CONICAL EXHAUST NOZZLESAIAA Journal, 1963
- Characteristics of Conical Supersonic NozzlesARS Journal, 1962
- The Static Hole Error ProblemAircraft Engineering and Aerospace Technology, 1962
- Truncated Perfect Nozzles in Optimum Nozzle DesignARS Journal, 1961
- Investigation of Supersonic Flow Separation in NozzlesJournal of Mechanical Engineering Science, 1959