Zobrazeno 1 - 10
of 15
pro vyhledávání: '"C L, Kirk"'
Publikováno v:
World review of nutrition and dietetics. 75
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=pmid________::ecb0097c14db6ca9d85ca69a980e2c8b
https://pubmed.ncbi.nlm.nih.gov/7871838
https://pubmed.ncbi.nlm.nih.gov/7871838
Autor:
C. L. Kirk, R. K. Jain
Publikováno v:
Journal of Energy Resources Technology. 103:41-47
The dynamic response of a double articulated structure to non-collinear Airey waves and a steady current is studied for various waves and varying current directions. The governing equations of motion are derived by Lagrange's method where wave and cu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7d5218e45d975fafbd98d2f56d6e24be
https://doi.org/10.1115/1.3230813
https://doi.org/10.1115/1.3230813
Autor:
D. M. Yourtee, C. L. Kirk-Yourtee
Publikováno v:
Journal of Toxicology: Toxin Reviews. 8:3-18
Studies to identify human aflatoxin metabolites provide essential information for understanding the clinical manifestations of these toxicants. Although there have been very few of these studies a total of 10 aflatoxins have been isolated from human
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::04175dda81297932e17ed69717a60d6e
https://doi.org/10.3109/15569548909059734
https://doi.org/10.3109/15569548909059734
Autor:
R. K. Jain, C. L. Kirk
Publikováno v:
The Aeronautical Journal. 78:32-36
The natural frequencies of a plate or a shell can be changed by altering its stiffness. This can be achieved by appropriately varying the mass or curvature, by introducing initial stresses or by attaching stiffeners to the system. The last method has
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f59a3ba8ee3c29140d22a023fd7969df
https://doi.org/10.1017/s0001924000036307
https://doi.org/10.1017/s0001924000036307
Autor:
C. L. Kirk
Publikováno v:
The Journal of the Royal Aeronautical Society. 67:799-803
SummaryThe response of an elastic system having a single degree of freedom, to a vibratory force whose waveform can be varied, is examined. The variable waveform is produced by a system of two pairs of unbalanced rotors in which one pair rotates at t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c6e12cf7841f2e80efe8bcf73564998f
https://doi.org/10.1017/s0001924000061674
https://doi.org/10.1017/s0001924000061674
Autor:
A. J. Pitt, C. L. Kirk
Publikováno v:
The Aeronautical Journal. 73:965-974
A VTOL aircraft which is in a state of hovering flight possesses no inherent stability of its own, consequently it may be found necessary to introduce some artificial form of control of the aircraft in both rolling and pitching motion. Such a control
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d18f7af016aab2beb08f901950859fee
https://doi.org/10.1017/s0001924000051411
https://doi.org/10.1017/s0001924000051411
Autor:
C. L. Kirk
Publikováno v:
The Aeronautical Journal. 75:476-483
The need to establish reliable methods of predicting the response of aircraft during taxying on rough runways and the associated dynamic loads and fatigue damage has led to numerous theoretical and experimental investigations of this problem. The pre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cc5c406cc8588a0d0f067bb202ed24fe
https://doi.org/10.1017/s0001924000045814
https://doi.org/10.1017/s0001924000045814
Autor:
C. L. Kirk
Publikováno v:
The Aeronautical Journal. 77:563-569
The purpose of this paper is to study the random vibration of linearly elastic, lumped-mass systems containing non-linear damping, to ideal stationary Gaussian white noise excitation.The following practical examples of systems with non-linear damping
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e164a27cb74876a169bc9e075328068b
https://doi.org/10.1017/s0001924000041890
https://doi.org/10.1017/s0001924000041890
Autor:
C. L. Kirk
Publikováno v:
Journal of Mechanical Engineering Science. 2:242-253
This paper describes methods of calculating natural frequencies of free flexural vibration of rectangular plates which have stiffeners parallel to one edge. An approximate frequency equation is derived for a clamped plate with closely spaced stiffene
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fb7a363e29d085a1a8b83c1bd51c9ab0
https://doi.org/10.1243/jmes_jour_1960_002_032_02
https://doi.org/10.1243/jmes_jour_1960_002_032_02
Autor:
C. L. Kirk
Publikováno v:
The Journal of the Royal Aeronautical Society. 65:695-697
Natural frequencies of free flexural vibration of rectangular plates may, in many cases, be considerably increased by attaching to the plate one or more elastic stiffening ribs parallel to one edge, or by casting or machining the plate and stiffeners
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0042ae6aa2cbb5fcb3ad32d208741bbf
https://doi.org/10.1017/s0368393100075544
https://doi.org/10.1017/s0368393100075544