Forced mixer lobes in ejector designs
- 1 July 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 4 (4) , 350-355
- https://doi.org/10.2514/3.23073
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Forced mixer lobes in ejector designsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- An approximate substitution principle for viscous heat conducting flowsProceedings of the Royal Society A: Mathematical, Physical and Engineering Sciences, 1985
- Turbofan Mixer Nozzle Flow Field—A Benchmark Experimental StudyJournal of Engineering for Gas Turbines and Power, 1984
- 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