Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Daniel F. Potter"'
Publikováno v:
International Journal of Aerospace Engineering, Vol 2012 (2012)
Numerical rebuilding of two trajectory points (t=1634 s and t=1643 s) of the Fire II mission has been carried out to predict the radiative heat flux for nonequilibrium and close-to-equilibrium conditions. The simulations have been performed with eilm
Externí odkaz:
https://doaj.org/article/dad8c12e0ee44fde84f972ceb05513bb
Space exploration missions may include atmospheric entries at very high velocities (for example, sample return or entries from hyperbolic orbits) or into an atmosphere with highly radiative constituents (for example, Mars or Titan). The effects of ga
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::ff48d2bac4afcbb81457d0de0399c6f4
https://doi.org/10.2514/1.a32791
https://doi.org/10.2514/1.a32791
Publikováno v:
Quarterly of Applied Mathematics. 60:707-736
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::74094d500a69ed34307c753cce7e5666
https://doi.org/10.1090/qam/1939008
https://doi.org/10.1090/qam/1939008
Publikováno v:
44th AIAA Thermophysics Conference.
This paper investigates the hypothesis that the observered gap between CFD and thermocouple-derived flight measurements for afterbody heating of the Viking spacecraft can be accounted for by infrared radiation from CO2 molecules in the wake flow. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::470d76d757bce64497cb2d54960fc156
https://doi.org/10.2514/6.2013-2895
https://doi.org/10.2514/6.2013-2895
Autor:
Stefan Löhle, Daniel F. Potter, Peter A. Jacobs, Andrew J. Neely, Neil Mudford, Ben Upcroft, Michael D. Jokic, Carolyn Jacobs, Troy N. Eichmann, Mary D'Souza, Peter Jenniskens, Timothy J. McIntyre, Hadas Porat, Razmi Khan, David R. Buttsworth
Publikováno v:
28th International Symposium on Shock Waves ISBN: 9783642256875
There are large uncertainties in the aerothermodynamic modelling of super-orbital re-entry which impact the design of spacecraft thermal protection systems (TPS). Aspects of the thermal environment of super-orbital re-entry flows can be simulated in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::31cc6b2a6f674d72a96353e16ffacacc
https://doi.org/10.1007/978-3-642-25688-2_5
https://doi.org/10.1007/978-3-642-25688-2_5