Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Kenneth E. Tatum"'
Publikováno v:
AIAA Journal. 57:4490-4503
High-speed local seeding particle injection for particle image velocimetry has been developed and demonstrated by measuring Mach 3 and Mach 10 turbulent boundary layers. The seeding injectors accel...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7f79fd9a7d937aefb805012b61a27767
https://doi.org/10.2514/1.j057654
https://doi.org/10.2514/1.j057654
Autor:
Kenneth E. Tatum, James S. Masters
Publikováno v:
AIAA Journal. 54:331-342
The Winslow elliptic smoothing equations have been shown to be effective for smoothing structured and unstructured computational meshes used in computational fluid dynamics applications. Although an implicit computational space is readily available f
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a04475905f3e350dff5da9223c0ff955
https://doi.org/10.2514/1.j054272
https://doi.org/10.2514/1.j054272
Autor:
Jason Klepper, James R. Sirbaugh, Kenneth E. Tatum, Stephen A. Guimond, Robert D. Knapke, James S. Masters, Derick Daniel
Publikováno v:
2018 Aerodynamic Measurement Technology and Ground Testing Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64da5fd165468acc043d979f8bc823eb
https://doi.org/10.2514/6.2018-3873
https://doi.org/10.2514/6.2018-3873
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c8b3722bb52e5707e58d9af24615abbd
https://doi.org/10.2514/6.2017-0272
https://doi.org/10.2514/6.2017-0272
Autor:
Lawrence D. Huebner, Kenneth E. Tatum
Publikováno v:
Journal of Aircraft. 30:571-577
Computational results are presented to illustrate the powered aftbody effects of representing the scramjet inlet on a generic hypersonic vehicle with a fairing, to divert the external flow, as compared to an operating flow-through scramjet inlet. Thi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::aa66c27f0b2a34e1992c40b061db5130
https://doi.org/10.2514/3.46384
https://doi.org/10.2514/3.46384
Autor:
Kenneth E. Tatum, Frederick L. Shope
Publikováno v:
23rd AIAA Applied Aerodynamics Conference.
A new procedure to design the contour of an axisymmetric hypersonic wind tunnel nozzle is presented. The method may be generally categorized as Navier-Stokes-based design by analysis. In the design procedure, the contour is first designed with an exi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ef86efed34b9b36570839c60062ccf07
https://doi.org/10.2514/6.2005-5081
https://doi.org/10.2514/6.2005-5081
Publikováno v:
37th AIAA Thermophysics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ff6f4b3eb5392fd375c3748d8f68317e
https://doi.org/10.2514/6.2004-2587
https://doi.org/10.2514/6.2004-2587
Publikováno v:
24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference.
Computational fluid dynamics techniques were applied in support of the conceptual design of an electric heater for obtaining true, or near-true, flight test conditions in a continuousflow Mach 7 wind tunnel without seriously vitiating the air. The ef
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f1bf80d47d2a781fc24e441fd8ddaf54
https://doi.org/10.2514/6.2004-2109
https://doi.org/10.2514/6.2004-2109
Autor:
John W. Slater, Kenneth E. Tatum
Publikováno v:
37th Aerospace Sciences Meeting and Exhibit.
The NPARC Alliance provides a publicly available, Internet based archive of analytical, experimental, and computational data suitable for validation of computational fluid dynamics (CFD) codes. The primary objective of the Archive is validation of th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f3224e895bbbc5d9899f7b00253db004
https://doi.org/10.2514/6.1999-747
https://doi.org/10.2514/6.1999-747
Autor:
Kenneth E. Tatum, Lawrence D. Huebner
Publikováno v:
22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference.
Computational results are presented for three issues pertinent to hypersonic, airbreathing vehicles employing scramjet exhaust flow simulation. The first issue consists of a comparison of schlieren photographs obtained on the aftbody of a cruise miss
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d8da696dc549c9ec052bc16ac8c582b1
https://doi.org/10.2514/6.1991-1709
https://doi.org/10.2514/6.1991-1709