Zobrazeno 1 - 10
of 143
pro vyhledávání: '"Hans G. Hornung"'
Autor:
Peter M. Finch, Julian J. Girard, Tal Schwartz, Christopher L. Strand, Ronald K. Hanson, Wesley M. Yu, Joanna M. Austin, Hans G. Hornung
Publikováno v:
AIAA Journal. 61:1555-1578
We report on measurements of rotational and vibrational temperature, velocity, and concentrations of nitric oxide (NO) in freestream flows at the T5 reflected shock tunnel at California Instistute of Technology. Quantities were measured at 50 kHz by
Autor:
Peter M. Finch, Tal Schwartz, Zev N. Granowitz, Wesley M. Yu, Thomas Gross, Christopher L. Strand, Thomas E. Schwartzentruber, Joanna M. Austin, Hans G. Hornung, Ronald K. Hanson
Publikováno v:
AIAA SCITECH 2023 Forum.
Publikováno v:
AIAA SCITECH 2022 Forum.
Autor:
Peter M. Finch, Tal Schwartz, Julian Girard, Wesley M. Yu, Christopher Strand, Joanna M. Austin, Hans G. Hornung, Ronald K. Hanson
Publikováno v:
AIAA SCITECH 2022 Forum.
Autor:
Joanna Austin, Christopher L. Strand, Ronald K. Hanson, Julian J. Girard, Wesley M. Yu, Hans G. Hornung, Peter Finch
This paper reports on measurements of freestream nitric oxide (NO) rotational and vibrational temperatures and partial pressures, collected in the Caltech T5 reflected shock tunnel. Quantum cascade lasers, emitting mid-infrared light resonant with fu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::cf46246aefc85bccbb66d48960bc27ba
https://resolver.caltech.edu/CaltechAUTHORS:20210910-224532781
https://resolver.caltech.edu/CaltechAUTHORS:20210910-224532781
Autor:
Peter Finch, Christopher L. Strand, Ronald K. Hanson, Wesley Y. Yu, Tal Schwartz, Julian J. Girard, Hans G. Hornung, Joanna Austin
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
Autor:
Joanna Austin, Peter Finch, Julian J. Girard, Ronald K. Hanson, Joel M. Lawson, Tal Schwartz, Hans G. Hornung, Christopher L. Strand, Wesley Y. Yu
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
Autor:
Hans G. Hornung
In a recent publication, Hornung et al. (J. Fluid Mech., vol. 871, 2019, pp. 1097–1116) showed that the shock wave stand-off distance and the drag coefficient of a cone in the inviscid hypersonic flow of a perfect gas can be expressed as the produc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8655196db7b061f30038082a634dc42a
https://resolver.caltech.edu/CaltechAUTHORS:20190923-091328424
https://resolver.caltech.edu/CaltechAUTHORS:20190923-091328424
Publikováno v:
Journal of Fluid Mechanics. 916
A computational parameter study of the viscous axisymmetric supersonic flow over a double cone is made with a view to determining the boundary of the region in which such flows are unsteady. The study is restricted to the case when the boundary layer
Publikováno v:
Journal of Fluid Mechanics. 871:1097-1116
Depending on the cone half-angle and the inverse normal-shock density ratio $\unicode[STIX]{x1D700}$, hypersonic flow over a spherically blunted cone exhibits two regimes separated by an almost discontinuous jump of the body end of the sonic line fro