Zobrazeno 1 - 10
of 50
pro vyhledávání: '"Seymour M. Bogdonoff"'
Publikováno v:
AIAA Journal. 30:1945-1952
A numerical study of the three-dimensional interaction between crossing shocks generated by symmetric sharp fins and a flat-plate turbulent boundary layer is presented. The full mean compressible Navier-Stokes equations, incorporating a turbulent edd
Publikováno v:
AIAA Journal. 30:890-896
The structure of the shock wave/turbulent boundary-layer interaction generated by a 3D swept compression corner has been investigated through a combined experimental and theoretical research program. The flowfield geometry is defined by the streamwis
Autor:
Seymour M. Bogdonoff
Publikováno v:
Proceedings of the First International Driving Symposium on Human Factors in Driver Assessment, Training and Vehicle Design: driving assessment 2001.
The BEI Driver Skill Enhancement Program (D-SEP) had its beginnings in a local group meeting to provide input to the White House Commission on Aging about 6 years ago. At this meeting, the author became acutely aware of the problems older people had
Autor:
Seymour M. Bogdonoff
Although hypersonics has been with us for over 50 years, the great advantages of very high speed flight have not been brought to engineering fruition. The present paper gives a brief overview of hypersonic flight, including the often neglected chemic
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::96880192c305063a487f22b7f54ae39b
https://doi.org/10.21236/ada370547
https://doi.org/10.21236/ada370547
Autor:
Sandrine Cogne, Joseph N. Forkey, Richard B. Miles, Walter R. Lempert, Alexander Smits, Seymour M. Bogdonoff
Publikováno v:
29th Joint Propulsion Conference and Exhibit.
Multiple pulsed Rayleigh imaging and filtered Rayleigh scattering are used to generate images of a complex boundary layer structure, shock wave/boundary layer interactions, and crossing shock waves. Time-sequenced Rayleigh images taken with a visible
Publikováno v:
29th Aerospace Sciences Meeting.
Three-dimensional interactions between crossing shock waves generated by symmetric sharp fins and a turbulent boundary layer on a flat plate are investigated experimentally and theoretically at Mach number 2.95 and freestream unit Reynolds number 1.9
Autor:
Seymour M. Bogdonoff
Publikováno v:
Separated Flows and Jets ISBN: 9783642844492
Modeling of the flowfield generated by the interaction of a shock wave and a turbulent boundary layer was carried out by using elements of a series of experiments and computations. Combining surface observations, flowfield surveys, and extensive comp
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff6b9026311e47a420b7d4db8a91709c
https://doi.org/10.1007/978-3-642-84447-8_38
https://doi.org/10.1007/978-3-642-84447-8_38
Autor:
Seymour M. Bogdonoff
Publikováno v:
Hypersonic Flows for Reentry Problems ISBN: 9783642845826
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9459bdd2a651bd6c6f930bdf2d898218
https://doi.org/10.1007/978-3-642-84580-2_3
https://doi.org/10.1007/978-3-642-84580-2_3
Autor:
Seymour M. Bogdonoff
Publikováno v:
28th Aerospace Sciences Meeting.