Modeling of the Performance of a F100-PW229 Equivalent Engine under Sea-Level Static Conditions
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Publisher
American Institute of Aeronautics and Astronautics
Reference11 articles.
1. 4Lee, A. S., Singh, R., and Probert, S. D. "Multi-Combustor Engines for Military Aircraft", 44thAIAA/ASME/SAE/ASEE JointPropulsion Conference and Exhibition, Hartford, CT, USA, 21 -23July2008.
2. Elements of Propulsion: Gas Turbines and Rockets
3. F100-PW-229 Higher Thrust in Same Frame Size
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