Vibration and flutter characteristics of a folding wing

Journal of Aircraft

Volumn 46, Issue 3, 2009, Pages 791-799

  Snyder, Matthew P ^a,d   Sanders, Brian ^b,d   Eastep, Franklin E ^c,d   Frank, Geoffrey J ^c,d  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c UNIVERSITY OF DAYTON RESEARCH INSTITUTE   (United States)

^d Building 146 ^*

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT ENVELOPES; FLUTTER (AERODYNAMICS);

DRIVE DESIGN; FINITE-ELEMENT APPROACH; FLUTTER INSTABILITY; FOLDING WINGS; GOLAND WING; MORPHING AIRCRAFTS; STRUCTURAL MODELING; VEHICLE WEIGHTS;

WINGS;

EID: 67650908705     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.34685     Document Type: Article

References (8)

1. Pace, S., "Valkyrie: North American XB-70," TAB Books, 2nd ed., Blue Ridge Summit, PA, 1990, chap. 3.
2. Pitt, D. M., "Static and Dynamic Aeroelastic Analysis of Structural Wing Fold Hinges That are Employed as an Aeroelastic Tailoring Tool," 45th AIAA/ASME/ASCE /AHS/ASC Structures, Structural Dynamics & Materials Conference, Palm Springs, California, 19-22 April 2004.
3. Livne, Eli., "Future of Airplane Aeroelasticity," Journal of Aircraft, Vol.40, No.6, 2003, pp. 1066-1092. doi:10.2514/2.7218
4. Snyder, M., Sanders, B., Frank, G., and Eastep, F., "Vibration and Flutter Characteristics of a Folding Wing," 46th AIAA/ASME/ASCE / AHS/ASC Structures, Structural Dynamics & Materials Conference, Austin, Texas, 18-21 April 2005.
5. Snyder, M., Sanders, B., Frank, G., and Eastep, F., "Sensitivity of Flutter to Fold Orientation and Spring Stiffness of a Simple Folding Wing," International Forum on Aeroelasticity and Structural Dynamics 2005, Munich, Germany, 28 June-1 July 2005.
6. Goland, M., "The Flutter of a Uniform Cantilever Wing," Journal of Applied Mechanics, Vol.12, No.4, Dec. 1945.
7. Arnaiz, H. H., Peterson, J. B., and Daugherty, J. C., "Wind-Tunnel/ Flight Correlation Study of Aerodynamic Characterisitcs of a Large Flexible Supersonic Cruise Airplane (XB-70-1)," NASA Technical Paper 1516, March 1980.
8. Love, H. H., Zink, P. S., Stroud, R. L., Bye, D. R., and Chase, C., "Impact of Actuation Concepts on Morphing Aircraft Structures," 45th AIAA/ASME/ASCE /AHS/ASC Structures, Structural Dynamics & Materials Conference, Palm Springs, California, 19-22 April 2004.