On the Deflection of Swept Cantilevered Surfaces

Martin, Harold C.

doi:10.2514/8.2125

Journal of the Aeronautical Sciences

1951

DOI: 10.2514/8.2125

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On the Deflection of Swept Cantilevered Surfaces

Harold C. Martin

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1952

1954

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Cited by 7 publications

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Estimation of the Effects of Distortion on the Longitudinal Stability of Swept Wing Aircraft at High Speeds (Sub-Critical Mach Numbers)

Campion¹

1954

Aeronautical Quarterly

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SummaryThe effects of distortion on the longitudinal stability of swept wing aircraft at high speeds (sub-critical Mach numbers) are considered on a quasi-static basis. The method is based on the theory of Gates and Lyon but involves some extension of this theory.The treatment of wing distortion is considered in some detail and the effects of built-in twist and camber and wing weight are included, using the so-called superposition method. The application of the analysis of Lyon and Ripley for investigating fuselage, tail and control circuit distortion is suggested, but means of modifying and simplifying this procedure where desirable are put forward.The analysis is illustrated by means of a simple example of a swept wing fighter aircraft for which wing, fuselage and tail distortion effects are considered, and the results are discussed with reference to the individual and combined distortion effects, as well as the effect of compressibility.

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Estimation of the Effects of Distortion on the Longitudinal Stability of Swept Wing Aircraft at High Speeds (Sub-Critical Mach Numbers)

Campion¹

1954

Aeronautical Quarterly

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An Initial Approach to the Overall Structural Problems of Swept Wings Under Static Loads

Sechler

1950

Journal of the Aeronautical Sciences

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For the past 2 l / 2 years, under the sponsorship of the Air Materiel Command of the U.S. Air Force, GALCIT has been investigating the subject of the stresses in thin swept wings. The investigation has utilized theoretical, experimental, and electrical agencies on this problem. The problem has been reduced to a form amenable to theoretical analysis by assuming the wing replaced by a thin cantilever plate of uniform thickness.

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A Review of Certain Analysis Methods for Swept-Wing Structures

Williams

1952

Journal of the Aeronautical Sciences

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On the Deflection of Swept Cantilevered Surfaces

Cited by 7 publications

References 2 publications

Estimation of the Effects of Distortion on the Longitudinal Stability of Swept Wing Aircraft at High Speeds (Sub-Critical Mach Numbers)

Estimation of the Effects of Distortion on the Longitudinal Stability of Swept Wing Aircraft at High Speeds (Sub-Critical Mach Numbers)

An Initial Approach to the Overall Structural Problems of Swept Wings Under Static Loads

A Review of Certain Analysis Methods for Swept-Wing Structures

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