Výsledky vyhledávání - "Matthew N. Rhode"

Estimation of Uncertainties for a Model Validation Experiment in a Wind Tunnel

Autor: Matthew N. Rhode, William L. Oberkampf

Publikováno v: Journal of Spacecraft and Rockets. 54:155-168

A high-quality model validation experiment was performed in the NASA Langley Research Center Unitary Plan Wind Tunnel to assess the predictive accuracy of computational-fluid-dynamics models for a blunt-body supersonic retropropulsion configuration a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::707463a46184e7c9bc0e57b2be37b3df
https://doi.org/10.2514/1.a33563

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Supersaturation Total Temperature, Pitot Pressure, and Rayleigh Scattering Measurements at Mach 10

Autor: Joel L. Everhart, R. Jeffrey Balla, Matthew N. Rhode

Publikováno v: AIAA Journal. 52:1452-1465

A fundamental research study of the supersaturation region is presented. This region is mapped in the NASA Langley 31-Inch Mach 10 Air Wind Tunnel freestream flow using physical probes (total temperature and pitot) and a nonintrusive offbody diagnost

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::a13c5dbcb80e4e04bf690a376b642b8a
https://doi.org/10.2514/1.j052608

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Supersonic Retropropulsion Validation Experiment in the NASA Langley Unitary Plan Wind Tunnel

Autor: Karl T. Edquist, Scott A. Berry, Matthew N. Rhode

Publikováno v: Journal of Spacecraft and Rockets. 51:664-679

The development of supersonic retropropulsion, an enabling technology for heavy payload exploration missions to Mars, is the focus of the present paper. A new experimental model, intended to provide computational fluid dynamics model validation data,

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::a4ba7cce98e4fa4cce6d30768e65bc9f
https://doi.org/10.2514/1.a32649

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Supersonic Retropropulsion Experimental Results from NASA Ames 9×7 Foot Supersonic Wind Tunnel

Autor: Karl T. Edquist, Matthew N. Rhode, Scott A. Berry

Publikováno v: Journal of Spacecraft and Rockets. 51:724-734

Supersonic retropropulsion was experimentally examined in the Ames Research Center 9×7 Foot Supersonic Wind Tunnel at Mach 1.8 and 2.4. The model, previously designed for and tested in the Langley Research Center Unitary Plan Wind Tunnel at Mach 2.4

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::c05ed483e4b946b64c9b9b542e475dcc
https://doi.org/10.2514/1.a32650

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Wind-Tunnel Results of the B-52B with the X-43A Stack

Autor: Mark C. Davis, Kevin D. Johnson, Alexander G. Sim, Matthew N. Rhode

Publikováno v: Journal of Spacecraft and Rockets. 44:871-877

A low-speed wind-tunnel test was performed with a 3%-scale model of a booster rocket mated to an X-43A research vehicle, a combination referred to as the Hyper-X launch vehicle. The test was conducted both in freestream air and in the presence of a p

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::d25d0f3157f7dc72fde86e55ba95975a
https://doi.org/10.2514/1.27191

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