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Nasa (Plant)
Known as:
Nasa
National Institutes of Health
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2017
2017
A CFD Case Study of a Fan Stage with Split Flow Path Subject to Total Pressure Distortion Inflow
Wai Ming To
2017
Corpus ID: 125257138
This report is the documentation of the work performed under the Hypersonic Project of the NASA’s Fundamental Aeronautics Program…
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2015
2015
Discussion of the NASA OCO-2 satellite measurements of CO₂ concentrations
A. Parker
2015
Corpus ID: 55969787
Recent papers and press releases have shown details of the latest results of the NASA OCO-2 experiment. Aim of this project is…
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2011
2011
Shuttle's end spells change at NASA
A. Witze
Nature
2011
Corpus ID: 205064375
As the shuttle flies its penultimate mission, the US space agency seeks to fill a looming gap in crew transport.
2011
2011
Flow Property Measurement Using Laser-Induced Fluorescence in the NASA Ames Interaction Heating Facility
J. Grinstead
,
B. Porter
,
J. Carballo
2011
Corpus ID: 96236666
The spectroscopic diagnostic technique of two photon absorption laser-induced fluorescence (TALIF) of atomic species has been…
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2002
2002
Aeroacoustic Experiments in the NASA Langley Low-Turbulence Pressure Tunnel
Meelan Choudhari
,
D. Lockard
,
+7 authors
M. Khorrami
2002
Corpus ID: 123095236
2002
2002
CFD ANALYSIS OF THE CIAM/NASA SCRAMJET
Allied Aerospace
2002
Corpus ID: 112432038
The CIAM/NASA flight test was numerically analyzed. The flowpath was divided into inlet and burner sections, and solved…
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1996
1996
···as NASA's claims win few converts
T. Reichhardt
Nature
1996
Corpus ID: 30709329
1988
1988
Aerodynamic performance and pressure distributions for a NASA SC(2)-0714 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel
R. Jenkins
,
A. S. Hill
,
E. J. Ray
1988
Corpus ID: 264280919
This report presents in graphic and tabular forms the aerodynamic coefficient and surface pressure distribution data for a NASA…
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1979
1979
Shuttle NASA payload integration
L. Williams
1979
Corpus ID: 107959838
The payload integration process of the Space Transportation System is described. A flight assignment process is outlined and…
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1971
1971
Wind-tunnel investigation of effects of trailing-edge geometry on a NASA supercritical airfoil section
C. D. Harris
1971
Corpus ID: 107241982
Wind-tunnel tests have been conducted at Mach numbers from 0.60 to 0.81 to determine the effects of trailing-edge geometry on the…
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