Computational fluid dynamics comparison and flight test measurement of F-5E off-body pressures

43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers

Volumn , Issue , 2005, Pages 7595-7604

  Meredith, Keith B ^a,d,e   Dahlin, John A ^a,d   Graham, David H ^a,d   Malone, Michael B ^a,d   Haering Jr , Edward A ^b,d,f   Page, Juliet A ^c,d,g   Plotkin, Kenneth J ^c,d,g  

^a NORTHROP GRUMMAN CORPORATION   (United States)

^b NASA DRYDEN FLIGHT RESEARCH CENTER   (United States)

^c WYLE LABORATORIES   (United States)

^d MZ 9V11/W6 ^*

^e AIAA   (United States)

^f MS 2228

^g Wyle Research Group   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT TESTS; SUPERSONIC SPEEDS; TAIL SHOCK; WING SHOCK;

COMPUTATIONAL FLUID DYNAMICS; CORRELATION METHODS; DATA ACQUISITION; SUPERSONIC AERODYNAMICS;

FLIGHT DYNAMICS;

EID: 30744469620     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. rd AIAA Aerospace Sciences Meeting and Exhibit, January 10-13, 2005, Reno, NV.
2. rd AIAA Aerospace Sciences Meeting and Exhibit, January 10-13, 2005, Reno, NV.
3. th Fluid Dynamics Conference, New Orleans, LA, June 17-20, 1996.
4. Pulliam, Thomas H., "Artificial Dissipation Models for the Euler Equations", AIAA-85-0438, 1985.
5. Tysinger, T.L., and Caughey, D.A., "Implicit Multigrid Algorithm for the Navier-Stokes Equations", AIAA-91-0242, 1991.
6. Page, J.A., and Plotkin, K, J., "An Efficient Method for Incorporating Computational Fluid Dynamics into Sonic Boom Prediction," AIAA-91-3275, September 1991.