Diffusers for supersonic intakes - The dependence of conical diffuser performance on inlet flow conditions
- 1 April 1979
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- The influence of compressor exit conditions on the performance of combustor-dump diffusersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Experiment on conical diffusers with distorted inflowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Some Effects on Conical Diffuser Performance of Preceding Normal Shock Boundary-Layer InteractionProceedings of the Institution of Mechanical Engineers, 1974
- Duct performance parameters considering spatially non-uniform flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972