Zobrazeno 1 - 10
of 14
pro vyhledávání: '"V. F. Chirkashenko"'
Publikováno v:
Journal of Engineering Physics and Thermophysics. 91:1110-1120
This paper is a review of the series of investigations carried out at the S. A. Khristianovich Institute of Theoretical and Applied Mechanics (ITAM, Siberian Branch of the Russian Academy of Sciences (RAS)) aimed at solving the sonic boom problem. It
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b95cc98eb57f9202e70acb9a64de0fb9
https://doi.org/10.1007/s10891-018-1838-4
https://doi.org/10.1007/s10891-018-1838-4
Publikováno v:
Quantum Electronics. 44:836-840
We report a study of the wave structure formed by an optical discharge plasma upon the absorption of repetitively pulsed CO{sub 2} laser radiation in a supersonic (M = 1.36) air flow. Experimental data are presented on the configuration of the head s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a9b5ba7d9923888f71e9a055014ed65d
https://doi.org/10.1070/qe2014v044n09abeh015410
https://doi.org/10.1070/qe2014v044n09abeh015410
Publikováno v:
Thermophysics and Aeromechanics. 20:669-678
Based on the analysis of various aspects of creating a supersonic transport aircraft of the second generation, the necessity of developing unconventional active methods of sonic boom level reduction is demonstrated. Surface cooling is shown to exert
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fd473f32d43ba8b30df009fa126b8e5e
https://doi.org/10.1134/s0869864313060036
https://doi.org/10.1134/s0869864313060036
Autor:
V. F. Chirkashenko
Publikováno v:
Measurement Techniques. 56:149-157
A method of measuring the parameters of supersonic flow with shock waves of arbitrary strength present in the flow is considered. An analytic relationship by means of which all the parameters of the disturbed flow may be determined with the use of a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c07bca03848d574135cd1a77d64570f9
https://doi.org/10.1007/s11018-013-0173-6
https://doi.org/10.1007/s11018-013-0173-6
Publikováno v:
AIP Conference Proceedings.
As a result of optical and pneumometric measurements is defined the flow shock wave structure that is formed by the optical breakdown, due to focused repetitively pulsed CO2 laser radiation when entering perpendicular to a supersonic (M = 1.36, 1.9)
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c359b07d262ca107c8f3d68bfc2f06d5
https://doi.org/10.1063/1.4964046
https://doi.org/10.1063/1.4964046
Publikováno v:
Thermophysics and Aeromechanics. 18:507-522
Results of numerical and experimental investigations of the sonic boom parameters for two configurations of civil supersonic transport are presented. Numerical modelling is performed by a combined method based on calculating the spatial flow in the n
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::71f5f48676b0eca706d8ed48fd8b1224
https://doi.org/10.1134/s0869864311040019
https://doi.org/10.1134/s0869864311040019
Publikováno v:
Journal of Applied Mechanics and Technical Physics. 50:284-290
The possibility of improving the efficiency of cryogenic forcing on the parameters of the hanging shock determining the length of the region of minimization of the sonic boom (middle zone) generated by a modified power-law body is studied. The effect
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aec7994be60bc13a92660d9637c0e2e3
https://doi.org/10.1007/s10808-009-0038-6
https://doi.org/10.1007/s10808-009-0038-6
Publikováno v:
Journal of Applied Mechanics and Technical Physics. 49:962-970
The possibility of controlling the sonic boom level by means of cooling the surface of a flying vehicle is discussed. The effect of surface cooling on the formation of the perturbed flow structure at large distances from the vehicle is demonstrated b
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c502a1669e102298d78aa4f9a14f8912
https://doi.org/10.1007/s10808-008-0119-y
https://doi.org/10.1007/s10808-008-0119-y
Publikováno v:
Journal of Engineering Physics and Thermophysics. 80:874-884
Results of numerical investigations of the influence of lift redistribution along the length of the airframe of an airplane arrangement on the parameters of the acoustic shock produced by this arrangement and its aerodynamic characteristics are prese
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1701c0b4cefac0d5763a5a126d99a892
https://doi.org/10.1007/s10891-007-0118-5
https://doi.org/10.1007/s10891-007-0118-5
Autor:
A. M. Kharitonov, V. I. Zvegintsev, V. F. Chirkashenko, D. Fletcher, S. V. Chibisov, S. Paris
Publikováno v:
Thermophysics and Aeromechanics. 13:489-497
Results on a hyperboloid-flare model tested in a new hypersonic wind tunnel with adiabatic compression AT-303 based at ITAM SB RAS at M∞ = 10 and 15 and in a wide range of Reynolds numbers are presented. Pressure and heat-flux distributions along t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e3e475dda1c4f870d926dee165f9b1d7
https://doi.org/10.1134/s0869864306040020
https://doi.org/10.1134/s0869864306040020