Unistructure—A New Concept for Light Weight Integrally Stiffened Skin Structure

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.54, Iss.4, 1993-12, pp. : 2-8

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

TANGO: Low cost light weight structure

By Vincendon M.

Air & Space Europe, Vol. 3, Iss. 3, 2001-05 ,pp. : 122-125

Elsevier

Access to resources Recommend Favorite

The Light Aeroplane Defined: New F.A.I. Regulations Regarding Weight Limits

Aircraft Engineering, Vol. 5, Iss. 2, 1993-12 ,pp. : 22-23

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Design for Minimum Weight: Considerations Based on the Long Wave Instability of Stiffened Plates in Compression

By A.F.I.A.S. S. Yusuff M.Sc. M.Ae.E. Dr.Ae.E. A.F.R.Ae.S.

Aircraft Engineering, Vol. 32, Iss. 10, 1993-12 ,pp. : 288-294

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Stressed-Skin Wooden Construction: Weight and Strength Compared with Aluminium Alloys

By Stepniewski W.

Aircraft Engineering, Vol. 15, Iss. 4, 1993-12 ,pp. : 110-112

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Stressed-Skin Wooden Construction: Weight and Strength Compared with Aluminium Alloys

By Stepniewski W.

Aircraft Engineering, Vol. 15, Iss. 5, 1993-12 ,pp. : 126-131

Emerald Group Publishing Ltd

Access to resources Recommend Favorite