Lift Correction for Finite Chord: A Method of Close Approximation that is not Laborious and is Applicable in General to Wings without Sweep

By D.Sc. J. Lockwood Taylor  

Aircraft Engineering, Vol. 22, Iss. 6, 1993-12 ,pp. : 174-174

Emerald Group Publishing Ltd

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Damage identification in a plate-like structure using modal data

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Aviation, Vol. 17, Iss. 2, 2013-06 ,pp. : 45-51

Taylor & Francis Ltd

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Calculation of Supersonic Aerodynamic Influence Matrices: A Numerical Method for Wings of Arbitrary Planform Suitable for Solution on the Digital Computer

By A.C.G.I. T.H. Hallstaff   B.Sc.  

Aircraft Engineering, Vol. 33, Iss. 1, 1993-12 ,pp. : 16-19

Emerald Group Publishing Ltd

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Aerodynamic Influence Coefficients for Delta Wings in Steady Supersonic Flow: A Method of Numerical Integration using Panels Bounded by Mach Lines

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Aircraft Engineering, Vol. 31, Iss. 1, 1993-12 ,pp. : 9-12

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Aeroelastic Problems of Low Aspect Ratio Wings: Part V. Application of the Structural and Aeroelastic Matrices to the Solution of Steady State Aeroelastic Problems

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Aircraft Engineering, Vol. 28, Iss. 6, 1993-12 ,pp. : 196-198

Emerald Group Publishing Ltd

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