Accession Number : ADP005856

Title :   Static Aeroelastic Considerations in the Definition of Design Loads for Fighter Airplanes,

Corporate Author : MESSERSCHMITT-BOELKOW-BLOHM G M B H MUNICH (GERMANY F R)

Personal Author(s) : Schmidinger, G. ; Sensburg, O.

Report Date : 03 OCT 1986

Pagination or Media Count : 20

Abstract : This paper first discusses some typical effects of static aeroelastic correction factors in context with the definition of structural design loads for major aircraft components. The influences on response parameters and resulting design loads are shown as well as the aeroelastic optimization of trailing edge flaps with respect to geometry, efficiency and hinge moments.

Descriptors :   *AEROELASTICITY, *AERODYNAMIC CONTROL SURFACES, AERODYNAMIC LOADING, STRUCTURAL COMPONENTS, STATICS, CORRECTIONS, AIRCRAFT, MATHEMATICAL MODELS, OPTIMIZATION, FLAPS(CONTROL SURFACES), WEST GERMANY.

Subject Categories : Aerodynamics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE