Computational investigation of slot blowing for fuselage forebody flow control

Aircraft Design

Volumn 2, Issue 1, 1999, Pages 45-63

  Murman, Scott M ^a   Rizk, Yehia M ^b   Cummings, Russell M ^c   Schiff, Lewis B ^b  

^a MCAT Institute   (United States)

^b NASA AMES RESEARCH CENTER   (United States)

^c CALIFORNIA POLYTECHNIC STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL METHODS; FLOW CONTROL; JETS; MATHEMATICAL MODELS;

OVERSET GRID METHOD; TANGENTIAL SLOT BLOWING;

FUSELAGES;

EID: 0032674155     PISSN: 13698869     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1369-8869(99)00006-3     Document Type: Article

References (23)

1. Bowers AH, Noffz GK, Peron LR. An aerodynamic and jet deflection model for thrust vectoring on the NASA F/A-18 High-Alpha Research Vehicle. NASA High-Angle-of-Attack Technology Conference, NASA Langley Research Center, October 1990.
2. Murri DG, Biedron RT, Erickson GE, Jordan FL, Hoffler KD. Development of actuated forebody strake controls for the F-18 High-Alpha Research Vehicle. NASA High-Angle-of-Attack Technology Conference, NASA Langley Research Center, October 1990.
3. Schreiner JA, Erickson GE, Guyton R. Application of tangential sheet blowing on the forebody of an F-18-like configuration for high-angle-of-attack maneuverability. NASA High-Angle-of-Attack Technology Conference, NASA Langley Research Center, October 1990.
4. Benek JA, Steger JL, Dougherty FC, Buning PG. Chimera: a grid embedding technique. AEDC-TR-85-64, 1986.
5. Tavella DA, Schiff LB, Cummings RM. Pneumatic vortical flow control at high angles of attack. AIAA Paper 90-0098, January 1990.
6. Yeh DT, Tavella DA, Roberts L, Fujii K. Numerical study of the effect of tangential leading edge blowing on delta wing vortical flow. AIAA Paper 89-0341, January 1989.
7. Logan AH. No tail rotor (NOTAR) design. Vertiflite 1989;35(3):28-30.
8. Steger JL. Implicit finite-difference simulation of flow about arbitrary two-dimensional geometries. AIAA Journal 1978;16(7):679-86.
9. Steger JL, Ying SX, Schiff LB. A partially flux-split algorithm for numerical simulation of compressible inviscid and viscous flow. Proceedings of a workshop on computational fluid dynamics. University of California, Davis, 1986.
10. Ying SX, Steger JL, Schiff LB, Baganoff D. Numerical simulation of unsteady, viscous, high angle of attack flows using a partially flux-split algorithm. AIAA Paper 86-2179, 1986.
11. Buning PG, Chiu IT, Obayashi S, Rizk YM, Steger JL. Numerical simulation of the integrated Space Shuttle vehicle in ascent. AIAA Paper 88-4359, August 1988.
12. Schiff LB, Cummings RM, Sorenson RL, Rizk YM. Numerical simulation of high-incidence flow over the F-18 fuselage forebody. Journal of Aircraft 1991;28(10): 609-17.
13. Tavella DA, Schiff LB, Gee K. Fighter yaw control at high incidence through fuselage blowing. NASA High-Angle-of Attack Technology Conference, NASA Langley Research Center, October 1990.
14. Rizk YM, Gee K. Numerical prediction of the unsteady flowfield around the F-18 aircraft at large incidence. AIAA Paper 91-0020, January 1991.
15. Baldwin B, Lomax H. Thin-layer approximation and algebraic model for separated turbulent flows. AIAA Paper 78-0257, January 1978.
16. Degani D, Schiff LB. Computation of turbulent supersonic flows about pointed bodies having crossflow separation. Journal of Computational Physics 1986;66:173-96.
17. Gee K, Tavella D, Schiff LB. Computational optimization of a pneumatic forebody flow control concept. AIAA Paper, 91-3249, September 1991.
18. Ghaffari F, Luckring J, Thomas J, Bates B. Navier-Stokes solution about the F/A-18 forebody-LEX configuration. AIAA Paper 89-0338, January 1989.
19. Narayanan MAB, Khadgi YN, Viswanath PR. Similarities in pressure distribution in separated flow behind backward-facing steps. Aeronautical Quarterly 1974;25:305-12.
20. Murman SM, Rizk YM, Cummings RM, Schiff LB. Computational investigation of slot blowing for fuselage forebody flow control. AIAA Paper 92-0020, January 1992.
21. Murman SM. Computational investigation of slot blowing for fuselage forebody flow control. M.S. Thesis, California Polytechnic State University, San Luis Obispo, CA, 1991.
22. Levy Y, Degani D, Seginer A. Graphical visualization of vortical flows by means of helicity. AIAA Journal 1990;28:1347-52.
23. Wood N, Nielson J. Circulation control airfoils - past, present, and future. AIAA Paper 78-0257, January 1978.