Summary of technology needs for high speed rotorcraft study-Reference-Cited by-同舟云学术

Summary of technology needs for high speed rotorcraft study

Published:1991-06-24 Issue: Volume: Page:
ISSN:
Container-title:27th Joint Propulsion Conference
language:
Short-container-title:

Author:

SCOTT MARK¹

Affiliation:

1. Sikorsky Aircraft, Stratford, CT

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-2148

Reference7 articles.

1. "Technical Evaluation of the Rotor Downwash Flow Field of the XV-15 Tilt Rotor", D.J. Harris, R.D. Simpson, NAVAL AIR TEST CENTER SY-14R-83, 1983.

2. "Folding Tilt Rotor Demonstrator Feasibility Study", J. V. Bowles. NASA Ames, 1986.

3. "Downwash Impingement Criteria for VTOL Aircraft", U.S. Army, Transportation Research Command, TRECOM Report 64-48, 1964.

4. "Comparisionof Outflows from a Helicopter, Tilt Wing and Jet Lift Hovering Aircraft". O.E. mi^ chaelsen, Canadair Limited/General Dynamics. AIAA Paper No. 71-992, 1971.

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