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Inlet-engine compatibility analysis

Published:1970-06-15 Issue: Volume: Page:
ISSN:
Container-title:6th Propulsion Joint Specialist Conference
language:
Short-container-title:

Author:

CAMPBELL J.¹,ELLIS S.¹

Affiliation:

1. UNITED AIRCRAFT CORP., PRATT AND WHITNEY AIRCRAFT DIV., WEST PALM BEACH, FLA.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1970-941

Reference5 articles.

1. A. W. Martin, "Propulsion System Flow Stability Program (Dynamic) Phase 11, Part VI Inlet Turbulence Scaling" Technical Report AFAPL-TR-69-113 Part VI, A i r Force Aero Propulsion Laboratory, Wright-Patterson A i r Force Base, February 1970.

2. Kulberg, J. F., D. E. Shepard, E. 0. King, and J. R. Ba!cer, "Dynamic Simulation of Turbine Engine Compressors," AIAA Paper No. 69-486.

Cited by 2 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. Flow Analysis of a Helicopter Engine Side Air Intake;Journal of Propulsion and Power;2017-09

2. The Dynamic Data Analyzer (DDA), an aircraft aero-propulsion digitalanalysis tool;21st Joint Propulsion Conference;1985-07-08

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