Aerodynamic Flight Test Results for the Adaptive Compliant Trailing Edge-Reference-Cited by-同舟云学术

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Aerodynamic Flight Test Results for the Adaptive Compliant Trailing Edge

Published:2016-06-10 Issue: Volume: Page:
ISSN:
Container-title:AIAA Atmospheric Flight Mechanics Conference
language:
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Author:

Cumming Stephen B.¹,Smith Mark S.¹,Ali Aliyah¹,Bui Trong T.¹,Ellsworth Joel¹,Garcia Christian A.²

Affiliation:

1. NASA Armstrong Flight Research Center

2. Jacobs

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-3855

Reference10 articles.

1. Analysis of Low-Speed Stall Aerodynamics of a Swept Wing with Seamless Flaps

2. An Overview of NASA’s SubsoniC Research Aircraft Testbed (SCRAT)

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