Full-scale wind-tunnel investigation of the effects of wing leading-edge modifications on the high angle-of-attack aerodynamic characteristics of a low-wing general aviation airplane-Reference-Cited by-同舟云学术

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Full-scale wind-tunnel investigation of the effects of wing leading-edge modifications on the high angle-of-attack aerodynamic characteristics of a low-wing general aviation airplane

Published:1980-08-04 Issue: Volume: Page:
ISSN:
Container-title:Aircraft Systems Meeting
language:
Short-container-title:

Author:

JOHNSON, JR. J.¹,NEWSOM W.¹,SATRAN D.¹

Affiliation:

1. NASA, Langley Research Center, Hampton, Va.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1980-1844

Reference13 articles.

Cited by 6 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. Investigation and Improvement of Stall Characteristic of High-Lift Configuration without Slats;International Journal of Aerospace Engineering;2019-11-26

2. Engineering analysis of drooped leading-edge wings near stall;Journal of Aircraft;1984-06

3. Errata: "A Computer System for Aircraft Flyover Acoustic Data Acquisition and Analysis";Journal of Aircraft;1984-06

4. Large-scale vortex-lattice model for the locally separated flow overwings;AIAA Journal;1982-12

5. An analytical technique for the analysis of airplane spin entry and recovery;20th Aerospace Sciences Meeting;1982-01-11

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