Zobrazeno 1 - 10
of 19
pro vyhledávání: '"A. H. Auslender"'
Publikováno v:
Journal of Propulsion and Power. 35:313-327
In dual-mode scramjet engines, the isolator comprises complex shock structures that provide the necessary compression of incoming air to sustain combustion farther downstream. This region of pressu...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::09a45b12c40a349388b6341a337b595a
https://doi.org/10.2514/1.b37175
https://doi.org/10.2514/1.b37175
Publikováno v:
Journal of Spacecraft and Rockets. 55:346-355
Analysis was performed to assess the impact of atmospheric-breathing supersonic retropropulsion as a technology solution for Mars descent. Vehicle models were developed for three architectures, emp...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b8bc3357947c8561cf0b4cf0cf41ebc7
https://doi.org/10.2514/1.a33959
https://doi.org/10.2514/1.a33959
Publikováno v:
AIAA Journal. 55:2888-2901
A dataset of normal shock trains in a rectangular cross-section channel has been created from direct numerical simulations in an effort to quantify the impact of inflow confinement ratio on the sho...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd9679f7c2bfb93c04447d8a8cdea0f8
https://doi.org/10.2514/1.j055333
https://doi.org/10.2514/1.j055333
Publikováno v:
Journal of Propulsion and Power. 32:574-582
Design and analysis of an atmospheric-breathing propulsion system to land large-scale spacecraft (10 + t) on Mars was performed. Mg-CO₂ propulsion feasibility was analytically investigated by employing equilibrium combustion simulations, finite-rat
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3079b7b9350421adb3b47e7367e65768
https://doi.org/10.2514/1.b35776
https://doi.org/10.2514/1.b35776
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::90b51e2155c1e15f1639498f696bc009
https://doi.org/10.2514/6.2016-1018
https://doi.org/10.2514/6.2016-1018
Autor:
Dale K. Ota, Ten-See Wang, Victor E. Pritchett, Aaron H. Auslender, Endwell O. Daso, Isaiah Blankson
Publikováno v:
AIAA Journal. 47:1313-1326
This study describes an active flow control concept that uses counterflowing jets to significantly modify external flowfields and strongly disperse the shock waves of supersonic and hypersonic vehicles to reduce aerothermal loads and wave drag. The p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dbb189cc385de020d98b44d5a25fbeea
https://doi.org/10.2514/1.30084
https://doi.org/10.2514/1.30084
Publikováno v:
50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8d5504d1c8e27a2a904f11a239cf4bc0
https://doi.org/10.2514/6.2014-3449
https://doi.org/10.2514/6.2014-3449
Publikováno v:
Journal of Propulsion and Power. 13:525-531
A study of kerosene combustion in a supersonic vitiated aire ow at Mach 4.75 e ight enthalpy was conducted in direct-connect tests at Mach 1.8 at a stagnation temperature of 1000 K. The effects of shockand vortex-enhanced mixing mechanisms on the com
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c9155406fd62647ee20e13e91eb3217c
https://doi.org/10.2514/2.5198
https://doi.org/10.2514/2.5198
Publikováno v:
Journal of Propulsion and Power. 10:841-847
A computational performance enhancement study was performed employing systematic modifications to a planarsidewall compression scramjet inlet operating at an entrance Mach number of 4 and at a dynamic pressure of 2040 psf. The variations included mod
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::279cc3ba15947c02ccee5e292374d759
https://doi.org/10.2514/3.23822
https://doi.org/10.2514/3.23822
Publikováno v:
16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference.
The propulsion research portfolio of the National Aeronautics and Space Administration Fundamental Aeronautics Program Hypersonics Project encompasses a significant number of technical tasks that are aligned to achieve mastery and intellectual stewar
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3bfa669f2d51af67e6b36dea88f219ab
https://doi.org/10.2514/6.2009-7277
https://doi.org/10.2514/6.2009-7277