Tilt rotor aeromechanics phenomena in low speed flight

AHS International 4th Decennial Specialists' Conference on Aeromechanics

Volumn , Issue , 2004, Pages 473-485

  Potsdam, Mark A ^a   Schaller, David F ^b   Rajagopalan, R Ganesh ^c   Silva, Mark J ^d  

^a US Army Aviat/Missile RD/EC   (United States)

^b Sukra Helitek   (United States)

^c Iowa State University   (United States)

^d LAC+USC Medical Center   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

PHYSICAL FIDELITY; PITCH-UP WITH SIDESLIP (PUWSS); ROTOR AEROMECHANICS; WIND SPEED;

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; CONTROL SYSTEMS; HELICOPTER ROTORS; MATHEMATICAL MODELS; MILITARY AVIATION; TURBULENCE; WIND EFFECTS;

FLIGHT DYNAMICS;

EID: 2942577707     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

1. th Annual Forum, Virginia Beach, VA, May, 2000.
2. McDonald, H. et al., "Tiltrotor Aeromechanics Phenomena: Report of Independent Assessment Panel-Final Report," November 2001.
3. Arrington, W.L., Kumpel, M., Marr, R.L., and McEntire, K.G., "XV-15 Tilt Rotor Research Aircraft Flight Test Data Report, Volume II of V: Performance and Handling Qualities," NASA CR 177406, June 1985.
4. th Annual Forum, Washington, DC, June 1988.
5. th Annual Forum, Montreal, Canada, June 2002.
6. Poling, D. R., Rosenstein, H, and Rajagopalan, R. G., "Use of a Navier-Stokes Code in Understanding Tiltrotor Flowfields in Hover," Journal of the American Helicopter Society, Vol. 43, No. 2, April 1998.
7. Meakin, R. L., "Unsteady Simulation of the Viscous Flow About a V-22 Rotor and Wing in Hover," AIAA Paper 95-3463, Atmospheric Flight Mechanics Conference, Baltimore, MD, August 1995.
8. Tai, T.C. and Vorwald, J., "Simulation of V-22 Rotorcraft Hover Flowfield," AIAA Paper 93-4878, 1993 AIAA International Powered Lift Conference, Santa Clara, CA, December 1993.
9. Felker, F., Shinoda, R., Heffernan, R., and Sheehy, H., "Wing Force and Surface Pressure Data from a Hover Test of a 0.658-Scale V-22 Rotor and Wing," NASA Technical Memorandum 102244, February 1990.
10. Johnson, W., "Calculation of Tilt Rotor Aeroacoustic Model (TRAM DNW) Performance, Airloads, and Structural Loads," Proceedings of the American Helicopter Society Aeromechanics Specialists' Meeting, Atlanta, GA, November 2000.
11. th Aerospace Sciences Meeting and Exhibit, Reno, NV, January 2001.
12. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January, 2000.
13. Rajagopalan, R. G. and Lim C. K., "Laminar Flow Analysis of a Rotor in Hover," Journal of the American Helicopter Society, Vol. 36, No. 1, 1991.
14. Patankar S. V., "Numerical Heat Transfer and Fluid Flow," Hemisphere Publishing Corporation, New York, 1980.