Forced mixer lobes in ejector designs
- 16 June 1986
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- An approximate substitution principle for viscous heat conducting flowsProceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, 1985
- Investigation of mixing in a turbofan exhaust duct. II Computer codeapplication and verificationAIAA Journal, 1984
- Evaluation of Hypermixing for Thrust Augmenting EjectorsJournal of Aircraft, 1974