In program carried out by McDonnell Aircraft Corp rudder on McDonnell F-4C aircraft was selected to demonstrate advantages of beryllium application; design considerations and analysis relating to rudder design loads, balance weight loads, panel flutter, thermal environment, rudder weight, buckling and crippling criteria; fabrication and assembly of beryllium structures; rudder test program consisting of element test and rudder ground test program using Be in selected areas.
Beryllium structures for aircraft
SAE -- Paper
SAE Meeting ; 1966 Beryllium
1966
11 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright Elsevier B. V. All rights reserved.
Beryllium Structures for Aircraft
SAE Technical Papers | 1966
|Beryllium and Beryllium Metal Matrix Composite Structures
British Library Conference Proceedings | 2001
|Beryllium Copper in the Aircraft Industry
Emerald Group Publishing | 1941
Beryllium for aerospace structures
Engineering Index Backfile | 1961
|