Zobrazeno 1 - 10
of 36
pro vyhledávání: '"J, Housner"'
Publikováno v:
The Aeronautical Journal. 118:181-196
This paper presents a novel analysis approach by considering multiple crack interaction in achieving FAA certification for durability and damage tolerance of exterior attachment installations on an aircraft fuselage according to FAA policy on Certifi
Publikováno v:
Advances in Composite Materials-Ecodesign and Analysis
The objective of this work is to provide the aerospace community with a robust computational capability to determine composite material strength allowables. The technical approach presented in this document serves two purposes: (1) reduce laminate le
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::35d6f2d99faad619e468da6af4042745
http://www.intechopen.com/articles/show/title/cost-effective-computational-approach-for-generation-of-polymeric-composite-material-allowables-for-
http://www.intechopen.com/articles/show/title/cost-effective-computational-approach-for-generation-of-polymeric-composite-material-allowables-for-
Autor:
J. Housner
Publikováno v:
1998 IEEE Aerospace Conference Proceedings (Cat. No.98TH8339).
A next generation rapid modeling, assembly and simulation design system is introduced. The design system utilizes smart component product models and smart tools. The concepts of the system, the smart models and the smart tools are discussed with succ
Publikováno v:
Surgery. 112(1)
Systemic oxygen delivery (DO2) is normally four to five times higher than oxygen consumption (VO2), and VO2 is independent of DO2. If DO2 is decreased to less than twice VO2, a state of anaerobic metabolism and supply dependency occurs. Some authors
Publikováno v:
Medicine & Science in Sports & Exercise. 34:S246
Publikováno v:
Medicine & Science in Sports & Exercise. 33:S182
Akademický článek
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Akademický článek
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Autor:
J. Housner, D. Weidman
Publikováno v:
25th Structures, Structural Dynamics and Materials Conference.
A selected list of references on the analysis of the deployment concepts for large space truss structures are reviewed. The stability of the deployment process is discussed, and stable methods of deployment mentioned. Analytical and experimental need
Autor:
J. Housner
Publikováno v:
25th Structures, Structural Dynamics and Materials Conference.
Convected-transient analysis techniques in the finite-element method are used to investigate the deployment and maneuver of large spacecraft structures with multiple-member flexible trusses and frames. Numerical results are presented for several samp