An experimental study of droop leading edge modifications on high and low aspect ratio wings up to 50 deg angle of attack-Reference-Cited by-同舟云学术

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An experimental study of droop leading edge modifications on high and low aspect ratio wings up to 50 deg angle of attack

Published:1993-08-09 Issue: Volume: Page:
ISSN:
Container-title:11th Applied Aerodynamics Conference
language:
Short-container-title:

Author:

GONZALEZ HUGO¹,WINKELMANN ALLEN¹

Affiliation:

1. Maryland Univ., College Park

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1993-3496

Reference23 articles.

1. Ellis, David R. "A Study of Light Plane Stall Avoidance and Suppression". Rep. No. FAA-RD-77-25,Feb. 1977

2. Feistel,T.W.; Anderson, S.B.; and Kroeger, R.A. "A Method of Localizing Wing Flow Separation at Stall to Alleviate Spin Entry Tendencies". AIM Paper 78-1476, Aug 1978.

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