Effect of a rotating propeller on the separation angle of attack-Reference-Cited by-同舟云学术

Effect of a rotating propeller on the separation angle of attack

Published:1993-01-11 Issue: Volume: Page:
ISSN:
Container-title:31st Aerospace Sciences Meeting
language:
Short-container-title:

Author:

BOLDMAN D.¹,IEK C.¹,HWANG D.¹,LARKIN M.²,SCHWEIGER P.²

Affiliation:

1. NASA, Lewis Research Center, Cleveland, OH

2. Pratt & Whitney Group, East Hartford, CT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-17

Reference15 articles.

1. Nacelle Aerodynamics Inlet Flow-Through High Angle of Attack Distortion Test," NASA CR-189149, July 1992. 3. Iek, C., Roldman, D.R., and Ibrahim, M. "Analysis

2. of an Advanced Ducted Propeller Subsonic Inlet," AIAA Paper 92-0274, Jan. 1992. 4. Ni, R.H. "A Multiple Grid Schemefor Solving the to the Free-Stream Direction," Journal of the

3. Computer Programs for Calculating Potential Flow in Propulsion System Inlets," NASA TM-73728, July 1977. 6. Smith, A.M.O., and Pierce, J. "Exact Solution of

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