Aerodynamic effects of an attitude control vane on a tilt-nacelle V/STOL propulsion system-Reference-Cited by-同舟云学术

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Aerodynamic effects of an attitude control vane on a tilt-nacelle V/STOL propulsion system

Published:1979-08-17 Issue: Volume: Page:
ISSN:
Container-title:Aircraft Systems and Technology Meeting
language:
Short-container-title:

Author:

BETZINA M.¹,KITA R.²

Affiliation:

1. NASA, Ames Research Center, Moffett Field, Calif.

2. Grumman Aerospace Corp., Bethpage, N.Y.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1979-1855

Reference24 articles.

1. 'Demers, W. J., Netzger, F. B., Smith, L. W., and Wainauski, 11. S . "Testing of the Hamilton Standard Q-Fan Demonstrator (Lycoming T55-L-llA Core Engine),'' NASA CR-121265, March 1973.

2. ' S h a i n , W. M. "Test Data Report, Low Speed [Mind Tunnel Tests of a F u l l Scale LiftiCruise - Fan Inlet, With Engine at High Angles of Attack,'' NASA CR-152072, J a n u a r y 1978.

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