Aerodynamics ofIntakes and Propelling NozzlesTheory and Design2Requirements made on the inlets and nozzles:Both1. Minimize installation drag on their own and adjacentaircraft surfaces over wide range of aircraft angle ofattack and engine throttle settings2. Maximize internal total pressure recovery (πd, πn ) ofIntake and nozzle individually under variousoperating conditions3. Provide controllabl ...[Show More]
Category: | Research Paper |
Number of pages: | 43 |
Language: | English |
Last updated: | 3 years ago |
Downloads: | 1 |
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