Static and dynamic aeroelastic analysis of structural wing fold hinges that are employed as an aeroelastic tailoring tool

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 2004, Pages 2654-2664

  Pitt, Dale M ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; AERODYNAMICS; ELASTICITY; HELICOPTERS; HINGES; STIFFNESS; STRUCTURAL DESIGN;

AEROELASTIC BENDING; AEROELASTIC TAILORING; AIRCRAFT DESIGN; WING FOLD HINGES;

WINGS;

EID: 16244410422     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (6)

1. Tripplet, W.E, Aeroelastic Tailoring Studies in Fighter Aircraft, AIAA 79-0725.
2. Weisshaar, T.A., "Aeroelastic Tailoring for Unconventional Aircraft Configurations", Presented at 2001 International Forum Aeroelasticity and Structural Dynamics, Volume I Plenary Lectures, pg 89-102.
3. Bohlmann, J.D., Eckstrom, C.V., Weisshaar, T.A." Aeroelastic Tailoring for Oblique Wing Lateral Trim", AIAA Paper 88-2263
4. Albano, E. and Rodden, W.P., A Doublet-Lattice Method for Calculating Lift Distributions on Oscillating Surfaces in Subsonic Flows, AIAA Journal, Vol. 7, No. 2, February 1969.
5. th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 12-15 April 1999, St. Louis, MO.
6. Pitt, D.M., The Use of Structural Wing Fold Hinges as an Aeroelastic Tailoring Tool, Presented at the International on Aeroelasticity and Structural Dynamics (IFASD), Amsterdam, June 4-6, 2003.