Aeroelastic analysis of advanced geometry tiltrotor aircraft

Journal of the American Helicopter Society

Volumn 43, Issue 3, 1998, Pages 212-221

  Srinivas, Venkataraman ^a,c   Chopra, Inderjit ^a   Nixon, Mark W ^b  

^a UNIVERSITY OF MARYLAND   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Engineering Technology Associates   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLUTTER (AERODYNAMICS); GEOMETRY; MATHEMATICAL MODELS; SPEED; TURBOMACHINE BLADES;

ROTOR BLADES; TILTROTOR AIRCRAFT;

HELICOPTER ROTORS;

EID: 0032119861     PISSN: 00028711     EISSN: None     Source Type: Journal    
DOI: 10.4050/jahs.43.212     Document Type: Article

References (8)

1. Gaffey, T.M., Yen, J.G., and Kvaternik, R.G., Analysis and Model Tests of the Proprotor Dynamics of a Tilt-Proprotor VTOL Aircraft, U.S. Air Force V/STOL Technology and Planning Conference, Las Vegas, Nevada, Sep 1969.
2. Kvaternik, R.G., Studies in Tilt-Rotor VTOL Aircraft Aeroelasticity, Ph.D. Dissertation, Case Western Reserve University, 1973.
3. Johnson, W., Dynamics of Tilting Proprotor Aircraft in Cruise Flight, NASA TN D-7677, May 1974.
4. Nixon, M.W., Aeroelastic Response and Stability of Tiltrotors with Elastically Coupled Composite Rotor Blades, Ph.D. Dissertation, University of Maryland, College Park, 1993.
5. Bir, G.S., and Chopra, I., Aeromechanical Stability of Rotorcraft with Advanced Geometry Blades, Proceedings of the 34th AIAA/ASME/ ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, LaJolla, CA, Apr 1993.
6. University of Maryland Advanced Rotorcraft Code (UMARC), Theory Manual, Center for Rotorcraft Education and Research, University of Maryland, College Park, MD, Jul 1994.
7. Srinivas, V., Aeroelastic Analysis of Advanced Tiltrotor Aircraft, Ph.D. Dissertation, University of Maryland, College Park, Maryland, 1995.
8. Johnson, W., Analytical Modeling Requirements for Tilting Proprotor Aircraft Dynamics, NASA TN D-8013, 1975.