The Effect of a Damping Compound on Jet-Efflux Excited Vibrations: An Article in Two Parts Presenting Theory and Results of Experimental Investigation PART I THE STRUCTURAL DAMPING DUE TO THE COMPOUND

By D.C.Ae. D.J. Mead  

Aircraft Engineering, Vol. 32, Iss. 3, 1993-12 ,pp. : 64-72

Emerald Group Publishing Ltd

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The Effect of a Damping Compound on Jet-Efflux Excited Vibrations: An Article in Two Parts Presenting Theory and Results of Experimental Investigation

By D.C.Ae. D.J. Mead  

Aircraft Engineering, Vol. 32, Iss. 4, 1993-12 ,pp. : 106-113

Emerald Group Publishing Ltd

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Tail Flutter—A New Theory: In which is Discussed in Some Detail the Structural Instability of Tail Planes at High Speed

By A.M.I.C.E. H. Bolas   M.B.E.   B.Sc.  

Aircraft Engineering, Vol. 1, Iss. 1, 1993-12 ,pp. : 16-22

Emerald Group Publishing Ltd

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Lift of a Two-Dimensional Cascade of Aerofoils: Simplified Method of Calculation Based on Schlichting's Theory

By M.Sc.(Eng.) J.J. Wannenburg   M.Sc.  

Aircraft Engineering, Vol. 32, Iss. 12, 1993-12 ,pp. : 350-355

Emerald Group Publishing Ltd

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Spar Web Buckling of a Supersonic Aircraft: An Analysis of a Simply-Supported Rectangular Plate Under the Action of In-Plane Stresses Due to the Action of Aerodynamic and Inertia Forces and Kinetic Heating Effects

By D.C.Ae. J.P.H. Webber   M.Sc. D.S. Houghton  

Aircraft Engineering, Vol. 35, Iss. 12, 1993-12 ,pp. : 364-368

Emerald Group Publishing Ltd

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