Simulation and analysis of V-22 tiltrotor aircraft forward-flight flowfield

Journal of Aircraft

Volumn 33, Issue 2, 1996, Pages 369-376

  Tai, Tsze C ^a,b  

^a NAVAL SURFACE WARFARE CENTER   (United States)

^b AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; FUSELAGES; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; THREE DIMENSIONAL; VISCOUS FLOW; VORTEX FLOW; WINGS;

ANGLE OF ATTACK; FLOW SEPARATION; FLOWFIELD; MACH NUMBER; TILTROTOR AIRCRAFT;

AIRCRAFT;

EID: 0030108210     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/3.46947     Document Type: Article

References (22)

1. McVeigh, M. A., Grader, W. K., and Paisley, D. J., "Rotor Airframe Interactions on Tiltrotor Aircraft," Journal of the American Helicopter Society, Vol. 35, No. 3, 1990, pp. 43-51.
2. Blohm, R., and Bartie, K., "V-22 Aerodynamic Report," Bell-Boeing Tiltrotor Team, Rept. 901-909-632, July 1986.
3. Felker, F. F., Shinoda, P. R., Hefferman, R. M., and Sheehy, H. F., "Wing Force and Surface Pressure Data from a Hover Test of a 0.658-Scale V-22 Rotor and Wing," NASA TM 10244, Feb. 1990.
4. Meyerhoff, C., and Gordge, D., "Navy Development Test (DT-IIA) of the MV-22 Aircraft, Contributory Test Report, Rotor Down-wash," Naval Air Test Center, Tech. Rept. RW-71R-90, Patuxent River, MD, 1990.
5. Grauer, W. K., and Farrell, M. K., "V-22 Flight Test Aerodynamics," Proceedings of the 47th Annual Forum of the American Helicopter Society, Vol. 1, American Helicopter Society, Washington, DC, 1991, pp. 101-106.
6. Schleicher, D. R., and Alexander, H. R., "Technology Development for Advanced Tiltrotor Transports," AIAA Paper 93-4810, Dec. 1993.
7. Raghavan, V, McCroskey, W. J., Van Dalsem, W. R., and Baeder, J. D., "Calculations of the Flow past Bluff Bodies, Including TiltRotor Wing Sections at a = -90 Deg," AIAA Paper 90-0032, Jan. 1990.
8. Fejtek, I., and Roberts, L., "Navier-Stokes Computation of Wing/ Rotor Interaction for a Tilt Rotor in Hover," AIAA Paper 91-0707, Jan. 1991.
9. Tai, T. C., and Vorwald, J., "Simulation of V-22 Rotorcraft Hover Flowfield," AIAA Paper 93-4878, Dec. 1993.
10. Meakin, R., "Moving Body Overset Grid Methods for Complete Aircraft Tiltrotor Simulations," AIAA Paper 93-3350, July 1993.
11. Sorenson, R. L., "The 3DGRAPE Book: Theory, Users' Manual, Examples," NASA TM 102224, July 1989.
12. Flores, J., and Hoist, T. L., "Numerical Solution of the Navier-Stokes Equations for Complex Configurations," Lecture Series in Computational Fluid Dynamics, Univ. of Tennessee Space Inst., Tulahoma, TN, March 1988.
13. Thomas, J. L., Krist, S. T, and Anderson, W. K., "Navier-Stokes Computations of Vortical Flows over Low-Aspect-Ratio Wings," AIAA Journal, Vol. 28, No. 2, 1990, pp. 205-212.
14. Baldwin, B., and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow," AIAA Paper 78-0257, Jan. 1978.
15. Spalart, P., and Allmaras, S., "A One-Equation Turbulence Model for Aerodynamic Flows," AIAA Paper 92-0439, Jan. 1992.
16. Rumsey, C. L., and Vatsa, V. N., "A Comparison of the Predictive Capabilities of Several Turbulence Models Using Upwind and Central-Difference Computer Codes," AIAA Paper 93-0192, Jan. 1993.
17. Degani, D., and Schiff, L. B., "Computation of Supersonic Viscous Flows Around Pointed Bodies at Large Incidence," AIAA Paper 83-0034, Jan. 1983.
18. Tai, T. C., "Theoretical Calculation of Viscous-Inviscid Transonic Flows," Lecture Series on Shock-Boundary Layer Interaction in Turbomachines, von Kármán Inst, for Fluid Dynamics, Brussels, Belgium, June 1980.
19. Jenks, M. D., and Narramore, J. C., "Final Report for the 2-D Test of Model 901 Rotor and Wing Airfoils (BSWT 592)," Bell-Boeing Tiltrotor Team, Rept. D901-99065-1, July 1984.
20. Visbal, M. R., "Onset of Vortex Breakdown Above a Pitching Delta Wing," AIAA Journal, Vol. 32, No. 8, 1994, pp. 1568-1575.
21. Tai, T. C., and Walker, M., "On Three-Dimensional Flow Separation Criteria," AIAA Paper 91-1740, June 1991.
22. Delery, J. M., "Physics of Vortical Flows," Journal of Aircraft, Vol. 29, No. 5, 1992, pp. 856-876.