Method for Analysis of V/STOL Aircraft Ejectors
Author:
Affiliation:
1. Textron Bell Aerospace, Buffalo, N. Y.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.59902
Reference13 articles.
1. 2Aerospace Applied Thermodynamics Manual, SAE, Warrendale, Pa., 1960.
Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Study of a circular cross section thrust augmenting ejector;29th Joint Propulsion Conference and Exhibit;1993-06-28
2. Advances in Ejector Thrust Augmentation;Recent Advances in Aerodynamics;1986
3. Application of thrusting ejectors to tactical aircraft having vertical lift and short-field capability;AIAA and NASA Ames VSTOL Conference;1981-08-17
4. Prediction of Performance of Low-Pressure-Ratio Thrust-Augmenter Ejectors;Journal of Aircraft;1978-12
5. Prediction Methods for Jet V/STOL Propulsion Aerodynamics;Journal of Aircraft;1978-02
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