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Alternate Subjects (1-16 of 16)
Pressure Distribution
1
E-Books/E-Docs
 

An airfoil flutter model suspension system to accommodate large static transonic airloads


Reed, Wilmer H.
Newport News, VA : DEI-Tech, Inc. ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:177998    ---  Available
2
E-Books/E-Docs
 

Application of laminar flow control to supersonic transport configurations



Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:181917    ---  Available
3
E-Books/E-Docs
 

Contraction design for small low-speed wind tunnels


Bell, J. H.
[Moffett Field, Calif.?] : National Aeronautics and Space Administration, Ames Research Center ; Stanford, CA : Stanford University, Joint Institute for Aeronautics and Acoustics, [1988] 1988

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:182747    ---  Available
4
Print Material
 

Design and use of a guided weight impactor to impart barely visible impact damage


Lovejoy, Andrew E., author.
Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, April 2016. 2016-

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 Axe Federal Documents Online  NAS 1.15:2016-218977    ---  Available
5
E-Books/E-Docs
 

Design concepts for cooled ceramic composite turbine vane


Boyle, Robert J., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, February 2015. 2015-

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:2015-218390    ---  Available
6
E-Books/E-Docs
 

Effects of velocity profile and inclination on dual-jet-induced pressures on a flat plate in a cross



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 1.26:177361    ---  Available
7
E-Books/E-Docs
 

Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speed


Plentovich, Elizabeth B.
[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 1.60:3099    ---  Available
8
E-Books/E-Docs
 

Enhanced design of turbo-jet LPT by separation control using phased plasma actuators


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

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:212294    ---  Available
9
E-Books/E-Docs
 

An experimental investigation of propfan installations on an unsewpt supercritical wing at transonic


Bartlett, Glynn R.
Hampton, Va. : Vigyan Research Associates, Inc. : National Aeronautics and Space Administration, Langley Research Center, [1985] 1985

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:172605    ---  Available
10
E-Books/E-Docs
 

Experimental investigation of unsteady flows at large incidence angles in a linear oscillating casca


Buffum, Daniel H., author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, July 1996. 1996-

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 Axe Federal Documents Online  NAS 1.15:107283    ---  Available
11
E-Books/E-Docs
 

The fast scattering code (FSC) validation studies and program guidelines


Tinetti, Ana Fiorella, 1962-
Hampton, Va : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

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 Axe Federal Documents Online  NAS 1.26:2011-217158    ---  Available
12
E-Books/E-Docs
 

Interaction of two-dimensional transverse jet with a supersonic mainstream


Kraemer, G. O.
Norfolk, Virginia : Department of Mechanical Engineering and Mechanics, School of Engineering, Old Dominion University ; Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 1983. 1983

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:175446    ---  Available
13
E-Books/E-Docs
 

Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic


Hall, Robert M., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, April 1979. 1979-

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:1385    ---  Available
14
E-Books/E-Docs
 

Prediction of sound fields in acoustical cavities using the boundary element method


Kipp, Carl R.
West Lafayette, Ind. : Ray W. Herrick Laboratories, School of Mechanical Engineering, Purdue University ; [Washington, DC : National Aeronautics and Space Administration, 1985] 1985

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:176295    ---  Available
15
E-Books/E-Docs
 

Solar rocket plume/mirror interactions


Yu, Sheng-Tao.
[Washington, D.C.] : National Aeronautics and Space Administration, [1991] 1991

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Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.26:185300    ---  Available
16
E-Books/E-Docs
 

Unsteady potential flow past a propeller blade section


Takallu, Mohammad Ali, 1948-
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 1.26:4307    ---  Available
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