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Alternate Subjects (1-20 of 20)
Turbulent Boundary Layer
1
E-Books/E-Docs
 

Aerothermal environment in chordwise gaps between split elevons at Mach 6.8


Hunt, L. Roane (Lewis Roane), author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:1783    ---  Available
2
E-Books/E-Docs
 

Boundary layer simulation improvement : progress report


Praharaj, Sarat C.
Huntsville, Ala. : Remtech, Inc. ; Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, George C. Marshall Space Flight Center, [1987] 1987

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:178845/2    ---  Available
3
E-Books/E-Docs
 

A critical evaluation of two-equation models for near wall turbulence


Speziale, C. G. (Charles G.), 1948-
Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995] 1990

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:182068    ---  Available
4
E-Books/E-Docs
 

Development of a defect stream function, law of the wall/wake method for compressible turbulent boun


Wahls, Richard A.
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:4286    ---  Available
5
E-Books/E-Docs
 

The effects of anisotropic free-stream turbulence on turbulent boundary layer behavior


Fang, Liang-Wei.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985] 1985

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:177379    ---  Available
6
E-Books/E-Docs
 

Enhanced viscous flow drag reduction using acoustic excitation final report


Nagel, R. T.
Hampton, Va. : NASA Langley Reasearch Center, [1988?] 1988

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 Axe Federal Documents Online  NAS 1.26:182734    ---  Available
7
E-Books/E-Docs
 

An estimation of turbulent kinetic energy and energy dissipation rate based on atmospheric boundary



Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information, [2000] 2000

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:210298    ---  Available
8
E-Books/E-Docs
 

Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hyper



[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : For sale by the National Technical Information Service], 1991. 1991

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:3142    ---  Available
9
E-Books/E-Docs
 

Flow separation in shock wave boundary layer interactions at hypersonic speeds


Hamed, A. (Awatef)
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service, 1990]. 1990

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:4274    ---  Available
10
E-Books/E-Docs
 

Fluctuating pressures measured beneath a high-temperature, turbulent boundary layer on a flat plate


Parrott, Tony L.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1989. 1989

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:2947    ---  Available
11
E-Books/E-Docs
 

Implementation of a transition model in a NASA code and validation using heat transfer data on a tur


Ameri, Ali A., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

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 Axe Federal Documents Online  NAS 1.26:2012-217436    ---  Available
12
E-Books/E-Docs
 

In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0


Quinn, Robert D., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November1980. 1980-

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:1764    ---  Available
13
E-Books/E-Docs
 

Interactive calculation procedures for mixed compression inlets


Reshotko, Eli.
Cleveland, Ohio : Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University, [1983] 1983

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 Axe Federal Documents Online  NAS 1.26:186581    ---  Available
14
E-Books/E-Docs
 

Inverse boundary-layer theory and comparsion with experiment


Carter, James E. (James Edward), 1944- author.
Washington, DC : National Aeronautics and Space Administration, Scientific and Technical Information Office, 1978. 1978

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 Axe Federal Documents Online  NAS 1.60:1208    ---  Available
15
E-Books/E-Docs
 

Modeling of turbulent boundary layer surface pressure fluctuation auto and cross spectra verificatio


Rackl, Robert.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2005] 2005

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 Axe Federal Documents Online  NAS 1.26:2005-213938    ---  Available
16
E-Books/E-Docs
 

Predicting modes of the unsteady vorticity field near the trailing edge of a blade


Devenport, William J.
[Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ; Hanover, MD : Available from NASA Center for Aerospace Information ; Springfield, VA : National Technical Information Service [distributor, 2003] 2003

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 Axe Federal Documents Online  NAS 1.26:212099    ---  Available
17
E-Books/E-Docs
 

A review of high-speed, convective, heat-transfer computation methods


Tauber, Michael E.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989. 1989

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 Axe Federal Documents Online  NAS 1.60:2914    ---  Available
18
E-Books/E-Docs
 

Risk assessment and scaling for the SLS LOx ET


Osipov, Viatcheslav (Slava), author.
Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, 2012. 2012

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 Axe Federal Documents Online  NAS 1.60:2012-216485    ---  Available
19
E-Books/E-Docs
 

Shock generation and control using DBD plasma actuators SBIR phase I final report


Patel, Mehul P., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

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 Axe Federal Documents Online  NAS 1.26:2012-217448    ---  Available
20
E-Books/E-Docs
 

Vortex/boundary-layer interaction semi-annual status report on research grant no. NAGW-581


Bradshaw, P. (Peter), 1935-
London : Imperial College of Science and Technology, Dept. of Aeronautics ; [Washington, D.C. : National Aeronautics and Space Administration, 1987] 1987

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:180255    ---  Available
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