Two-Spar Wing Stress Analysis: A Method Taking into Account the Finite Spacing of the Ribs, with Detailed Numerical Calculations and Test Results for a Model Wing Test Specimen

Author： Goodey W.J.  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.21, Iss.11, 1993-12, pp. : 358-361

Disclaimer: Any content in publications that violate the sovereignty, the constitution or regulations of the PRC is not accepted or approved by CNPIEC.

Previous Menu Next

Abstract

Related content

Two-Spar Wing Stress Analysis: A Method Taking into Account the Finite Spacing of the Ribs, with Detailed Numerical Calculations and Test Results for a Model Wing Test Specimen

By Goodey W.J.  

Aircraft Engineering, Vol. 21, Iss. 10, 1993-12 ,pp. : 313-319

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Two-Spar Wing Stress Analysis: The Mathematical Theory, with Numerical Examples

By A.F.R.Ae.S. W.J. Goodey   M.A.  

Aircraft Engineering, Vol. 15, Iss. 1, 1993-12 ,pp. : 2-7

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Two-Spar Wing Stress Analysis: A Theory Giving a Reasonable Approximation to the Stress-Distribution in a Skin-Covered Plane

By A.F.R.Ae.S. W.J. Goodey   M.A.  

Aircraft Engineering, Vol. 13, Iss. 6, 1993-12 ,pp. : 150-153

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Wing Download Results from a Test of a 0.658-Scale V-22 Rotor and Wing

By Felker Fort F.  

Journal of the American Helicopter Society, Vol. 37, Iss. 4, 1992-10 ,pp. : 58-63

AHS International

Access to resources Recommend Favorite

Application of the Finite Element Method to Rotary-Wing Aeroelasticity

By Friedmann P. P.   Straub F.  

Journal of the American Helicopter Society, Vol. 25, Iss. 1, 1980-01 ,pp. : 36-44

AHS International

Access to resources Recommend Favorite