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Alternate Subjects (1-24 of 24)
Aerodynamics
1
ElectronicResource GovDoc
 

Aerodynamic design of a propeller for high-altitude balloon trajectory control


Eppler, Richard, author.
Greenbelt, Maryland : National Aeronautics and Space Administration, Goddard Space Flight Center, 2012. 2012

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 Axe Federal Documents Online  NAS 1.26:2012-215893    ---  Available
2
ElectronicResource GovDoc
 

Autonomous momentum management for space station final report, 15 October 1984



Huntsville, Ala. : George C. Marshall Space Flight Center, [1984] 1984

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 Axe Federal Documents Online  NAS 1.26:174065    ---  Available
3
ElectronicResource GovDoc
 

Design of a slotted, natural-laminar-flow airfoil for business-jet applications


Somers, Dan M.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012] 2012

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 Axe Federal Documents Online  NAS 1.26:2012-217559    ---  Available
4
Electronic Book
 

Dynamic modeling of starting aerodynamics and stage matching in an axi-centrifugal compressor


Wilkes, Kevin, author.
Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center : U.S. Army Research Laboratory, October 1996. 1996-

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 Axe Federal Documents Online  NAS 1.15:107338    ---  Available
5
ElectronicResource GovDoc
 

The effects of inlet turbulence and rotor/stator interactions on the aerodynamics and heat transfer


Dring, Robert P.
East Hartford, Conn. : United Technologies Research Center ; [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1988] 1988

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 Axe Federal Documents Online  NAS 1.26:179469    ---  Available
6
ElectronicResource GovDoc
 

The effects of Reynolds number, motor incidence angle and surface roughness on the heat transfer dis


Blair, M. F.
East Hartford, Conn. : United Technologies Research Center ; [Marshall Space Flight Center, Ala. : National Aeronautics and Space Administration, Goerge C. Marshall Space Flight Center ; Springfield, Va. : National Technical Information Service, distributor, 1991] 1991

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 Axe Federal Documents Online  NAS 1.26:187693    ---  Available
7
ElectronicResource GovDoc
 

Enhancement/upgrade of Engine Structures Technology Best Estimator (EST/BEST) software system


Shah, Ashwin.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2003] 2003

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 Axe Federal Documents Online  NAS 1.26:2003-212126    ---  Available
8
Electronic Book
 

Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with w


McLallin, Kerry L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, October 1980. 1980-

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 Axe Federal Documents Online  NAS 1.60:1730    ---  Available
9
Electronic Book
 

Flight dynamics principles


Cook, M. V.
London : Arnold ; New York : J. Wiley, 1997. 1997

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 Axe Elsevier ScienceDirect Ebook  Electronic Book    ---  Available
10
Electronic Book
 

Flight dynamics principles : a linear systems approach to aircraft stability and control


Cook, M. V.
Waltham, MA : Butterworth-Heinemann, ©2013. 2013

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 Axe Elsevier ScienceDirect Ebook  Electronic Book    ---  Available
11
Electronic Book
 

Ice accretions and full-scale iced aerodynamic performance data for a two-dimensional NACA 23012 air


Addy, Harold E., Jr., 1960- author.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, April 2016. 2016-

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 Axe Federal Documents Online  NAS 1.60:2016-218348    ---  Available
12
Electronic Book
 

The International Vehicle Aerodynamics Conference


International Vehicle Aerodynamics Conference (2014 : Holywell Park, Loughborough, Great Britain)
Cambridge, UK : Woodhead Publishing, 2014. 2014

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 Axe Elsevier ScienceDirect Ebook  Electronic Book    ---  Available
13
Electronic Book
 

Inverse boundary-layer theory and comparison 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
14
Electronic Book
 

Leading-edge deflection optimization for a highly swept arrow-wing configuration


Coe, Paul L., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-

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 Axe Federal Documents Online  NAS 1.60:1777    ---  Available
15
Print Material
 

Let's fly a plane! : launching into the science of flight with aerospace engineering


Ferrie, Chris, author.
Naperville, Illinois : Sourcebooks Explore, [2020] 2020

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 Pittsburg 1st Fl Juvenile Non-Fiction  J 629.132 Fer    ---  Available
16
ElectronicResource GovDoc
 

Missile aerodynamics for ascent and re-entry


Watts, G. L., author.
Huntsville, Alabama : National Aeronautics and Space Administration, Langley Research Center, 2012. 2012

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 Axe Federal Documents Online  NAS 1.26:2012-217475    ---  Available
17
ElectronicResource GovDoc
 

Modeling of vortex-induced oscillations based on indicial response approach


Truong, Khiem Van.
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1990] 1990

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 Axe Federal Documents Online  NAS 1.26:186560    ---  Available
18
ElectronicResource GovDoc
 

Numerical study of three-dimensional separation and flow control at a wing-body junction progress re


Lakshmanan, Balakrishnan, 1957-
Norfolk, Va. : Department of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

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 Axe Federal Documents Online  NAS 1.26:185819    ---  Available
19
Electronic Book
 

Optimal regulation in systems with stochastic time sampling


Montgomery, Raymond C., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980. 1980-

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 Axe Federal Documents Online  NAS 1.60:1743    ---  Available
20
ElectronicResource GovDoc
 

Prediction of forces and moments for flight vehicle control effectors



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

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 Axe Federal Documents Online  NAS 1.26:186572    ---  Available
21
ElectronicResource GovDoc
 

Semi-annual status report on NASA grant NAG 1-1087 "identification of aerodynamic models for maneuve


Chin, Suei.
Lawrence, Kan. : Flight Research Laboratory, The University of Kansas Center for Research, Inc., [1990] 1990

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 Axe Federal Documents Online  NAS 1.26:186630    ---  Available
22
Electronic Book
 

Stability boundaries for systems with frequency-model feedback and complementary filter


Barker, L. Keith, author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980. 1980-

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 Axe Federal Documents Online  NAS 1.60:1744    ---  Available
23
ElectronicResource GovDoc
 

Testing, analysis, and code verification of aerodynamics and heat transfer related to turbomachinery


King, Paul I.
[Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center ; Springfiled, Va. : For sale by the National Technical Information Service, 1991] 1991

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 Axe Federal Documents Online  NAS 1.26:188640    ---  Available
24
ElectronicResource GovDoc
 

Unsteady aero computation of a 1 1/2 stage large scale rotating turbine


To, Wai-Ming.
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012] 2012

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 Axe Federal Documents Online  NAS 1.26:2012-217438    ---  Available
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