Zobrazeno 1 - 10
of 183
pro vyhledávání: '"C L, Kirk"'
Autor:
H. Saunders
Publikováno v:
The Shock and Vibration Digest. 16:36-37
Autor:
Huang, Jia-hui1 (AUTHOR), Lei, Chun-yu1 (AUTHOR), Shen, Ya-lun1 (AUTHOR), Tian, En-jing1 (AUTHOR) tianenjing66@163.com
Publikováno v:
MycoKeys. 2024, Issue 109, p171-185. 15p.
Publikováno v:
World review of nutrition and dietetics. 75
Autor:
Antonín, Vladimír1 (AUTHOR) vantonin@mzm.cz, Ďuriška, Ondrej2 (AUTHOR), Jančovičová, Soňa3 (AUTHOR), Kudláček, Tomáš4 (AUTHOR), Para, Roberto5 (AUTHOR), Ševčíková, Hana1 (AUTHOR), Tomšovský, Michal4 (AUTHOR)
Publikováno v:
Systematics & Biodiversity. Dec2023, Vol. 21 Issue 1, p1-25. 25p.
Autor:
González‐Alemañy, Eduardo1 (AUTHOR) eduardog@cneuro.edu.cu, Rodríguez Olivera, Anelin Dayris2 (AUTHOR), Bobes, María Antonieta1 (AUTHOR), Armony, Jorge L.3,4 (AUTHOR)
Publikováno v:
European Journal of Neuroscience. Nov2023, Vol. 58 Issue 10, p4255-4263. 9p.
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
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
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
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
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