Motion induced unsteady aerodynamic loads with development of vortical flow

Author:

Wiggen Stefan1,Klein Christian1,Henne Ulrich1,Konrath Robert1,Sachs Werner1,Wrede Björn1,Nuhn Johannes1,Büte Thomas1,Mai Holger1

Affiliation:

1. German Aerospace Center (DLR)

Publisher

American Institute of Aeronautics and Astronautics

Reference40 articles.

1. 1Babister, A. “Flutter and Divergence of Swept-back and Swept-forward Wings,” A.R.C. Technical Report, (13,391) 2761, Aeronautical research council, 1953.

2. 2Barmby, J., Cunningham, H., and Garrick, I. “Study of effects of sweep on the flutter of cantilever wings,” Tech. Rep. REPORT 1014, National advisory committee for aeronautics, 1951.

3. Recent developments in delta wing aerodynamics

4. The unsteady aerodynamics of slender wings and aircraft undergoing large amplitude maneuvers

5. Low Speed Wind Tunnel Tests on the 1303 UCAV Concept

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