论飞机强度规范的发展

Abstract

Abstract: In this paper the historical evolution of american military aircraft strength specifica- tion,the speciality charactestics of the Aircraft Structure General Specification MIL-A-87221 of USAF and the relationship between MIL-A-87221 and MIL-A-8860 Serial Specifications of Aircraft Strength and Rigidity Specifications are Stated.By understanding american specifica- tions and analyzing the recent status of our aircraft development and strength specification,it is demonstrated that our future specification should be the further development of Military Aircraft Strength and Rigidity Specification GJB67.1～13-85 which should be substituted after the issue and application of the new specification. Finally,its adaptation scope and technical way of com- pilation are mentioned.

Key words: aircraft design structural design criteria, aircraft structure

CLC Number:

Jiang Zuguo;Wang Ji;QuJianzhong;WangGenyuan;ZhangYonghe. ON THE DEVELOPMENT OF AIRCRAFT STRENGTH SPECIFICATION[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 1994, 15(1): 1-7.

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ON THE DEVELOPMENT OF AIRCRAFT STRENGTH SPECIFICATION

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