Zobrazeno 1 - 10
of 10
pro vyhledávání: '"W. C. Crisman"'
Autor:
W. C. Crisman, Billy J. Harris
Publikováno v:
Journal of the Engineering Mechanics Division. 91:93-111
Two methods are presented for predicting face-wrinkling failure stresses for edgewise loaded sandwich panels. One method, based on Forest Products Laboratory theoretical parameters, is for the specialized case of fiberglas-facing, aluminum-honeycomb-
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fbd7590d5ad18e52e0cb92f8792a2a45
https://doi.org/10.1061/jmcea3.0000629
https://doi.org/10.1061/jmcea3.0000629
Publikováno v:
AIAA Journal. 7:250-257
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::df3d98aafc7f65fe2014b6d9c0121fa1
https://doi.org/10.2514/3.5082
https://doi.org/10.2514/3.5082
Publikováno v:
Journal of Aircraft. 5:27-34
This paper reports the initial investigations on full-size sandwich shell structures consisting of cylindrically curved panels and full cylinders, although some previous work in fabrication and basic buckling tests on small flat panels is presented a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::d34441f7067c3a54f5d1bc180365fbad
https://doi.org/10.2514/3.43903
https://doi.org/10.2514/3.43903
Publikováno v:
Journal of Engineering for Industry. 89:662-670
This paper is a theoretical and experimental study of the effect of core shear flexibility on the lowest natural frequency, node locations, and damping in sandwich beams with cores of high shear flexibility as exemplified by honeycomb-type cores. A n
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d1bebbf554d4230a204f393f20642839
https://doi.org/10.1115/1.3610130
https://doi.org/10.1115/1.3610130
Autor:
Gene M. Nordby, W. C. Crisman
Contributions to the acceptance of fiberglass-reinforced plastic (FRP) as an aircraft structural material were made through verification of existing theoretical strength relationships by the fabrication and testing of sandwich panels in the laborator
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c25e3f9df05422aa302b1e927abcb566
https://doi.org/10.21236/ad0621522
https://doi.org/10.21236/ad0621522
Autor:
Gene Nordby, W. C. Crisman
A survey of Army aircraft structural failures caused by corrosion, Fatigue, and abrasion was made to define critical areas of future structural research. The primary source of data was the Army failure reports, 'Equipment Improvement Recommendation'.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::430f7f1d66b51500105285fd59cf1426
https://doi.org/10.21236/ad0605325
https://doi.org/10.21236/ad0605325
The research covered in this report involves investigation of the effects of raw materials usage and fabrication process variables on the final strength properties of fiberglass-reinforced plastic (FRP) sandwich structure suitable for use as a primar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5a632ae8b820f46d4100f30d6419a69
https://doi.org/10.21236/ad0607339
https://doi.org/10.21236/ad0607339
Publikováno v:
Journal of Engineering for Industry. 89:443-444
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a347b63b7779192e4fe97776ab0120bf
https://doi.org/10.1115/1.3610080
https://doi.org/10.1115/1.3610080
Autor:
W. C. Crisman, Billy J. Harris
Publikováno v:
Journal of the Engineering Mechanics Division. 92:103-104
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3725fd7fc44d1ca6cc782565650a57b8
https://doi.org/10.1061/jmcea3.0000760
https://doi.org/10.1061/jmcea3.0000760
Publikováno v:
AIAA Journal. 7:1824a-1824a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2768e83bb0918bb81b4998df9a925cd7
https://doi.org/10.2514/3.55519
https://doi.org/10.2514/3.55519