Zobrazeno 1 - 10
of 78
pro vyhledávání: '"George R. Inger"'
Autor:
James N. Moss, George R. Inger
Publikováno v:
AIAA Journal. 45:2102-2106
A N IMPORTANT feature of hypersonicflight vehicleflowfields is shock/boundary layer interaction, and in laminar flow this often provokes a sizable region of separation followed by reattachment. Accordingly, CFD tools are under development for predict
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::476104b4dcdb4b02ffda32d77d585371
https://doi.org/10.2514/1.28278
https://doi.org/10.2514/1.28278
Autor:
George R. Inger
Publikováno v:
Progress in Aerospace Sciences. 43:42-63
The short-ranged local viscous–inviscid interaction field generated by a wall temperature jump on a flat plate in supersonic flow is studied in detail with an analytical triple-deck model. Treatment of the rapid heat transfer changes both upstream
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b7543692052cde88edc43aa65c78abc5
https://doi.org/10.1016/j.paerosci.2007.05.003
https://doi.org/10.1016/j.paerosci.2007.05.003
Autor:
George R. Inger
Publikováno v:
AIAA Journal. 43:706-715
Prologue O N 7 May 1940—a year and a half before Pearl Harbor—test pilot Woodward Burke climbed into a specially instrumented Brewster XF2A-2 experimental Navy fighter (Fig. 1), took off from Langley Field at 6 a.m. and headed for a remote area o
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b80060f877440e76c5d9dfddd38f5152
https://doi.org/10.2514/1.5025
https://doi.org/10.2514/1.5025
Autor:
R. L. Baker, George R. Inger
Publikováno v:
Journal of Spacecraft and Rockets. 42:193-200
An approximate yet accurate analysis of aerodynamic heating at a highly cooled stagnation region, which embraces the entire high-altitude hypersonic flight regime where nonequilibrium dissociation/recombination in the shock layer and finite surface c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d902ba0b8dff6b499e10d257b443c7be
https://doi.org/10.2514/1.7568
https://doi.org/10.2514/1.7568
Autor:
George R. Inger
Publikováno v:
Journal of Thermophysics and Heat Transfer. 18:108-113
An approximate analytical theory of the onset of viscous effects on hypersonic-body nose shock standoff distance is developed. Boundary-layer displacement, shock layer vorticity, and longitudinal curvature effects are all included, as are the influen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e5d62624fb5101d29a32c39de8641c09
https://doi.org/10.2514/1.9157
https://doi.org/10.2514/1.9157
Autor:
Holger Babinsky, George R. Inger
Publikováno v:
AIAA Journal. 40:1567-1573
The effect of surface roughness and step changes of surface roughness on an unseparated incipient shockwave/turbulent boundary-layer interaction has been studied using complementary experimental and theoretical investigations. Step changes in surface
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e8c07620ffb4b3ef7724e1002cf1c1f6
https://doi.org/10.2514/2.1825
https://doi.org/10.2514/2.1825
Publikováno v:
Journal of Thermophysics and Heat Transfer. 16:245-250
This paper presents a new theory of hypersonic blunt-nose shock standoff, based on a compressibility coordinate transformation for inviscid flow. It embraces a wide range of nonequilibrium shock-layer chemistry and gas mixtures including ionization a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::13874460ffcdc5e18ac5c504ce44964b
https://doi.org/10.2514/2.6674
https://doi.org/10.2514/2.6674
Autor:
George R. Inger
Publikováno v:
Journal of Spacecraft and Rockets. 38:185-190
Damks personal background is e rst outlined, followed by an examination of his early pioneering work in the 1930s on reacting e ows, which led to the basic nondimensional similitude parameters that now bear his name. We then survey the role that thes
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1db22294193f0a04d7af60fecbc6fb53
https://doi.org/10.2514/2.3692
https://doi.org/10.2514/2.3692
Autor:
Holger Babinsky, George R. Inger
Publikováno v:
Journal of Aircraft. 37:1028-1032
Many aerodynamic flow control devices make use of wall transpiration as a means of influencing boundary-layer behavior. The use of drilled-hole plates has come to be preferred for this purpose. To evaluate the aerodynamic performance of such plates i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fdf0d7b94bf4c71cb7f84b05c757dcb0
https://doi.org/10.2514/2.2707
https://doi.org/10.2514/2.2707
Autor:
George R. Inger
Publikováno v:
Journal of Thermophysics and Heat Transfer. 13:379-382
A fundamental asymptotic analysis of the subject problem is given based on a triple deck model, here generalized to include both gas phase nonequilibrium dissociation and arbitrary surface catalycity. This theory provides several important results. F
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::733e73c5b64e181667e90323b978dd31
https://doi.org/10.2514/2.6450
https://doi.org/10.2514/2.6450