Structural Aspects of Swept-Back Wings: An Account of Research Work in Sweden, with Particular Reference To Model Tests

By Grad.I.Mech.E. B.R. Noton   D.C.Ae.   Grad. R.Ae.S.  

Aircraft Engineering, Vol. 25, Iss. 11, 1993-12 ,pp. : 330-343

Emerald Group Publishing Ltd

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Elastic Instability of a Swept Panel: Analysis of the Buckling Tendency of a Panel of the Top Skin of a Swept Wing

By M.A. E.H. Mansfield  

Aircraft Engineering, Vol. 24, Iss. 2, 1993-12 ,pp. : 48-49

Emerald Group Publishing Ltd

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Aeroelastic Problems of Low Aspect Ratio Wings: Part I. Structural Analysis

By Thomann G.E.A.  

Aircraft Engineering, Vol. 28, Iss. 2, 1993-12 ,pp. : 36-42

Emerald Group Publishing Ltd

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Tapered Spar Frames: An Approximate Method for the Determination of the Stresses in, and Deflections of, a Fuselage

By B.Sc. H.M.J. Kittelsen   D.I.C  

Aircraft Engineering, Vol. 13, Iss. 4, 1993-12 ,pp. : 90-94

Emerald Group Publishing Ltd

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The Direct Stress Anal/sis of Swept Cantilever Plates of Low Aspect Ratio: An Approximate Method, employing the Principle of Least Work, which Obviates the Need for Intermediate Deflection Calculations

By A.F.R.Ae.S. A. Coull   B.Sc.(Eng.)   D.C.Ae.   Ph.D.  

Aircraft Engineering, Vol. 37, Iss. 6, 1993-12 ,pp. : 182-190

Emerald Group Publishing Ltd

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