Navier-Stokes Solutions for an Axisymmetric Nozzle
- 1 September 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (9) , 1219-1227
- https://doi.org/10.2514/3.51183
Abstract
No abstract availableThis publication has 14 references indexed in Scilit:
- Numerical simulation of three-dimensional boattail afterbody flow fieldsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Numerical simulation of multi-stream nozzle flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Numerical simulation of the interaction of jet and freestream flows in engine exhaust systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A patched solution of the transonic flowfield about an axisymmetric boattailPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Transonic flow over afterbodies including the effects of jet-plume and viscous interactions with separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Mach Reflection Associated with Over-Expanded Nozzle Free Jet FlowsAIAA Journal, 1975
- Mach Disk from Underexpanded Axisymmetric Nozzle FlowAIAA Journal, 1974
- Mach disk in underexpanded exhaust plumesAIAA Journal, 1971
- LOCATION OF THE NORMAL SHOCK WAVE IN THE EXHAUST PLUME OF A JETAIAA Journal, 1963
- On the Structure of Jets from Highly Underexpanded Nozzles Into Still AirJournal of the Aerospace Sciences, 1959