Microstructural changes that drilling and reaming can cause in the bore holes in DTD 5014 (RR58 extrusions)

Author： AIM P.J.E. FORSYTH  

Publisher： Emerald Group Publishing Ltd

ISSN： 0002-2667

Source： Aircraft Engineering, Vol.44, Iss.11, 1993-12, pp. : 20-23

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

Simplifying the Drilling of Marked Off Holes

By Moore H.  

Aircraft Engineering, Vol. 19, Iss. 11, 1993-12 ,pp. : 366-366

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

The Development of Hiduminium-RR.58 Aluminium Alloy: The background to the choice of the main structural material for Concorde

By Doyle W.M.  

Aircraft Engineering, Vol. 41, Iss. 11, 1993-12 ,pp. : 11-14

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

The Strength of Alclad D.T.D. 390

By B.Sc. I.G. Bowen  

Aircraft Engineering, Vol. 17, Iss. 8, 1993-12 ,pp. : 240-241

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Introduction to Designing With Aluminium Extrusions in Today's Aircraft

By  

Aircraft Engineering, Vol. 65, Iss. 11, 1993-12 ,pp. : 2-4

Emerald Group Publishing Ltd

Access to resources Recommend Favorite

Official D.T.D. Specifications: The Latest List of Requirements Called for by The Air Ministry Technical Department

By  

Aircraft Engineering, Vol. 4, Iss. 3, 1993-12 ,pp. : 72-72

Emerald Group Publishing Ltd

Access to resources Recommend Favorite