Aeroelastic tailoring - Theory, practice, and promise

Aeroelastic tailoring technology is reviewed with reference to the historical background, the underlying theory, current trends, and specific applications. The specific application discussed include the Transonic Aircraft Technology program, an Advanced Design Composite Aircraft, the Wing/Inlet Advanced Development program, and the forward-swept wing. Finally, the future of aeroelastic tailoring and the development of an aeroelastic tailoring analysis and design tool under the Automated Strength-Aeroelastic Design program are examined.

[1]  Jr. N. Krone Divergence elimination with advanced composites , 1975 .

[2]  F. R. Shanley,et al.  Weight-strength analysis of aircraft structures , 1960 .

[3]  E. Crawley,et al.  Vibration of Cantilevered Graphite/Epoxy Plates With Bending-Torsion Coupling , 1982 .

[4]  D. Gimmestad Aeroelastic tailoring of a composite winglet for KC-135 , 1981 .

[5]  R. Hearmon,et al.  The significance of coupling between shear and extension in the elastic behaviour of wood and plywood , 1943 .

[6]  M. Price,et al.  Aeroelastically tailored wing design , 1980 .

[7]  D Young,et al.  Vibration of rectangular plates by the Ritz method , 1950 .

[8]  W. J. Dwyer,et al.  Aeroelastically Tailored Propellers , 1977 .

[9]  S. Tsai,et al.  Introduction to composite materials , 1980 .

[10]  William Fuller Brown,et al.  Interpretation of Torsional Frequencies of Crystal Specimens , 1940 .

[11]  Holt Ashley,et al.  On Making Things the Best-Aeronautical Uses of Optimization , 1982 .

[12]  William E. Triplett,et al.  Aeroelastic Tailoring Studies in Fighter Aircraft Design , 1979 .

[13]  John A. Green,et al.  Aeroelastic tailoring of aft-swept high-aspect-ratio composite wings , 1987 .

[14]  T. J. Hertz,et al.  Wind Tunnel Demonstration of Aeroelastic Tailoring Applied to Forward Swept Wings , 1981 .

[15]  Stephen M. Batill,et al.  FASTOP: A Flutter and Strength optimization Program for Lifting-Surface Structures , 1977 .

[16]  John Dugundji,et al.  Experimental aeroelastic behavior of forward-swept graphite/epoxy wings with rigid-body freedom , 1987 .

[17]  F. Austin,et al.  AEROELASTIC TAILORING OF ADVANCED COMPOSITE LIFTING SURFACES IN PRELIMINARY DESIGN , 1976 .

[18]  T. Weisshaar Aeroelastic Tailoring of Forward Swept Composite Wings , 1981 .

[19]  Waddoups,et al.  The Vibration Response of Laminated Orthotropic Plates , 1965 .

[20]  J. V. Nagaraja,et al.  Vibration of Rectangular Plates , 1953 .

[21]  T. A. Weisshaar,et al.  Control of aeroelastic instabilities through stiffness cross-coupling , 1986 .

[22]  E. H. Mansfield,et al.  The Fibre Composite Helicopter Blade , 1979 .

[23]  L. A. Schmit,et al.  Structural synthesis - Its genesis and development , 1981 .

[24]  E. F. Crawley,et al.  Frequency determination and non-dimensionalization for composite cantilever plates , 1980 .

[25]  M. E. Waddoups,et al.  Analysis of Anisotropic Plates , 1969 .

[26]  Terrence A. Weisshaar,et al.  VIBRATION AND FLUTTER OF ADVANCED COIIPOSITE LIFTING SURFACES , 1983 .

[27]  T. A. Weisshaar,et al.  Vibration Tailoring of Advanced Composite Lifting Surfaces , 1985 .

[28]  Terrence A. Weisshaar Divergence of Forward Swept Composite Wings , 1980 .

[29]  Joel Markowitz,et al.  An Efficient Structural Resizing Procedure for Meeting Static Aeroelastic Design Objectives , 1978 .

[30]  W. Triplett,et al.  Aeroelastic tailoring of a forward swept wing and comparisons with three equivalent aft swept wings , 1980 .