Perspectives on rotorcraft aerodynamic modeling for flight dynamics applications

AHS International 4th Decennial Specialists' Conference on Aeromechanics

Volumn , Issue , 2004, Pages 731-740

  Kothmann, Bruce D ^a   Lu, Yi ^a   DeBrun, Erik ^a   Horn, Joe ^b  

^a BOEING COMPANY   (United States)

^b PENNSYLVANIA STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BERNOULLI EQUATION; BOUND CIRCULATION; UNSTEADY RESPONSE;

AIRFOILS; COMPUTATIONAL METHODS; COMPUTER SIMULATION; FLIGHT DYNAMICS; FLOW VISUALIZATION; VORTEX FLOW; VORTEX SHEDDING; WAKES;

HELICOPTER ROTORS;

EID: 2942545976     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (17)

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2. Chen, R.T.N., "A Survey of Nonuniform Inflow Models for Rotorcraft Flight Dynamics and Control Applications," Vertica, 14:2, pp. 147-184, 1990.
3. Peters, D.A., and HaQuang, N., "Dynamic Inflow for Practical Applications," AHS Journal, 33, pp. 63-68, 1988.
4. th AHS Forum, Washington, DC, 2001.
5. Curtiss, Jr., H.C., and Quackenbush, T., "Influence of the Rotor Wake on Rotorcraft Stability and Control", ERF 1988.
6. Chen, R.T.N., and Hindson, W.S., "Influence of Dynamic Inflow on the Helicopter Vertical Response," Vertica, 11:1, pp. 77-91, 1989.
7. Curtiss, Jr., H.C., and Shupe, N.K., "A Stability and Control Theory for Hingeless Rotors," 27 AHS Forum, Washington, DC, 1971.
8. th AHS Forum, Montreal, Canada, 2002.
9. Harris, F.D., "Articulated Rotor Blade Flapping Motion at Low Advance Ratio," AHS Journal, pp. 41-48, 17:1, 1972.
10. nd AHS Forum, Washington, DC, 1996.
11. th AHS Forum, Phoenix, AZ, 2003.
12. Wittmer, K., "Rotorcraft Airspeed Measurement without a Static Pressure Source," 2003.
13. Prouty, R.W., "Development of the Empennage Configuration of the YAH-64 Advanced Attack Helicopter," USAAVRADCOM-TR-82-D-22, 1983.
14. Stiles, L., et al., "Comanche Tail Feathers -Code or Tin?" Society of Experimental Test Pilots Meeting, 2001.
15. nd AHS Forum, Washington, DC, 1996.
16. Gessow, A., and Myers, G.C., Aerodynamics of the Helicopter, College Park Press, 1952.
17. Carpenter, P.J., and Fridovich, B., "Effect of a Rapid Blade-Pitch Increase on the Thrust and Induced Velocity Response of a Full-Scale Helicopter-Rotor" NACA TN 3044, 1953.