Fluid Mechanism of Wing Rock for Configurations with Chine-Shaped Forebodies-Reference-Cited by-同舟云学术

Fluid Mechanism of Wing Rock for Configurations with Chine-Shaped Forebodies

Published:2002-10 Issue:4 Volume:15 Page:125-135
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Saad Ahmed A.¹,Liebst Brad S.²,Gordnier Raymond E.³

Affiliation:

1. Postdoctorate Research Fellow, Air Force Inst. of Technology/ENY, Bldg. 640, 2950 P St., WPAFB, OH 45433.

2. Professor and Department Head, Air Force Inst. of Technology/ENY, Bldg. 640, 2950 P St., WPAFB, OH 45433.

3. Research Aerospace Engineer, Air Force Research Lab./VAAC, Bldg. 146, 2210 8 St., WPAFB, OH 45433.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%290893-1321%282002%2915%3A4%28125%29

Reference17 articles.

1. AGARD. (1991). “Computation aerodynamics based on Euler equations.” Tech. Rep. AGARD-AG-325 NATO Research and Technology Agency Nevilly Sur Seine France.

2. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations

3. Brandon J. M. and Nguyen L. T. (1986). “Experimental study of effects of forebody geometry on high angle of attack static and dynamic stability.” AIAA Paper No. 86-0331 AIAA Reston Va.

4. Erickson G. E. and Brandon J. M. (1985).“Low-speed experimental study of the vortex flow effects of a fighter forebody having unconventional cross-section.” AIAA Paper No. 85-1798 AIAA Reston Va.

5. Ericsson L. E. (1987). “Wing rock generated by forebody vortices.” AIAA Paper No. 87-0268 AIAA Reston Va.