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

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

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 trai...

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Bibliographische Detailangaben
Hauptverfasser: Schmidinger, G, Sensburg, O
Format: Report
Sprache:eng
Schlagworte:
AERODYNAMIC CONTROL SURFACES
AERODYNAMIC LOADING
Aerodynamics
AEROELASTICITY
AIRCRAFT
Component reports
CORRECTIONS
FLAPS(CONTROL SURFACES)
Fluid Mechanics
MATHEMATICAL MODELS
OPTIMIZATION
STATICS
STRUCTURAL COMPONENTS
Structural loads
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Beschreibung
Zusammenfassung: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. This article is from 'Static Aeroelastic Effects on High Performance Aircraft', AD-A199 170, p3-1 thru 3-20.