Zobrazeno 1 - 8
of 8
pro vyhledávání: '"David W. Witte"'
Autor:
Stephen J. Alter, Greg J. Brauckmann, Matthew N. Rhode, David W. Witte, James C. Ross, Bryan E. Falman, Karl T. Edquist, Thomas K. West, William L. Kleb, Mark Schoenenberger
Publikováno v:
AIAA AVIATION 2021 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::206ec2a8258aed45dd70c0b18a83acca
https://doi.org/10.2514/6.2021-2961
https://doi.org/10.2514/6.2021-2961
Publikováno v:
12th AIAA International Space Planes and Hypersonic Systems and Technologies.
An experimental study was performed to examine jet-effects for an airframe-integrated, scramjet-rocket combined-cycle vehicle configuration at transonic test conditions. This investigation was performed by testing an existing exhaust simulation wind
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::666f91e3c04c6041116f7c2bb549f11c
https://doi.org/10.2514/6.2003-7001
https://doi.org/10.2514/6.2003-7001
Publikováno v:
39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8e0263fa08eda916db3b3f14e206751d
https://doi.org/10.2514/6.2003-4406
https://doi.org/10.2514/6.2003-4406
Publikováno v:
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::591b41bb97984bf5a05ab4b8ed3cbe9d
https://doi.org/10.2514/6.2000-3605
https://doi.org/10.2514/6.2000-3605
Autor:
Luther R. Gartrell, Cecil E. Nichols, William W. Hunter, William M. Humphreys, David W. Witte
Publikováno v:
New Trends in Instrumentation for Hypersonic Research ISBN: 9789401048071
A fluidized bed seeding system for the injection of Aluminum Oxide into a Mach 6 flow field is described. Laser transit anemometer tests verified the operational capability of the seeding system. Measurements across an oblique shock with a two-compon
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9e3b4eeadf5195e77d2b8c76808bcb13
https://doi.org/10.1007/978-94-011-1828-6_31
https://doi.org/10.1007/978-94-011-1828-6_31
Publikováno v:
29th Aerospace Sciences Meeting.
An experimental study of an axial-compression interior-corner region with shock impingement was conducted in the NASA Langley 20-inch Mach 6 Tunnel to obtain aerodynamic heating rate distributions. The model, a generic hypersonic engine inlet, had a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ea5a858b020d787976d1d616f1685674
https://doi.org/10.2514/6.1991-527
https://doi.org/10.2514/6.1991-527
Publikováno v:
2nd International Aerospace Planes Conference.
Experimental and computational results are presented for a generic scramjet nozzle/afterbody model. Mixtures of argon and Freon were employed as simulant scramjet exhaust gases because they correctly model the inviscid simulation parameters of actual
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::771160ae621b00e6686dea1b8fc37edd
https://doi.org/10.2514/6.1990-5242
https://doi.org/10.2514/6.1990-5242
Publikováno v:
Journal of Spacecraft and Rockets. 29:288-289
References ^ohen, R. B., Penn, J. P., Janson, S. W., Lichtin, D. A., Zondervan, K. P., Sharp, L. R., Thaller, L. H., and DeVincenzi, D. L., "Preliminary Concepts for a Solar Electric Orbit Raising Experiment,''AIAA Paper 89-2373, July 1989. Rosen, S.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::07abe18942f1624bed8491f78af598f6
https://doi.org/10.2514/3.26347
https://doi.org/10.2514/3.26347