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Aerofoils

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1.
Rotational augmentation on a 2.3 MW rotor blade with thick flatback airfoil cross-sections : preprint
Author
Schreck, S.
Published
[Golden, Colo.] : National Renewable Energy Laboratory, 2013.
Online
http://purl.fdlp.gov/GPO/gpo36863
Location
Yale Internet Resource >> None
Format
Books / Online
2.
Applications of circulation control technologies
Published
Reston, VA : American Institute of Aeronautics and Astronautics, ©2006.
Online
Online book
Location
Yale Internet Resource >> None
Format
Books / Online
3.
Applications of circulation control technologies
Published
Reston, Va. : American Institute of Aeronautics and Astronautics, c2006.
Online
Online book
Location
Yale Internet Resource >> None
Format
Books / Online
4.
Computational study of large droplet breakup in the vicinity of an airfoil final report
Published
Washington, D.C. : U.S. Dept. of Transportation, Federal Aviation Administration, Office of Aviation Research, [2005]
Online
http://purl.access.gpo.gov/GPO/LPS66081
Location
Yale Internet Resource >> None
Format
Books / Online
5.
Wind turbine post-stall airfoil performance characteristics guidelines for blade-element momentum methods preprint
Author
Tangler, James L.
Published
Golden, Colo. : National Renewable Energy Laboratory, [2004]
Online
http://purl.access.gpo.gov/GPO/LPS70697
Location
Yale Internet Resource >> None
Format
Books / Online
6.
Wind tunnel aeroacoustic tests of six airfoils for use on small wind turbines preprint
Author
Migliore, Paul G.
Published
Golden, Colo. : National Renewable Energy Laboratory, [2003]
Online
http://purl.access.gpo.gov/GPO/LPS51700
Location
Yale Internet Resource >> None
Format
Books / Online
7.
Theory of wing sections : including a summary of airfoil data
Author
Abbott, Ira H.
Published
Mineola : Dover Publications, [1999], ©1959.
Online
Online book
Location
Yale Internet Resource >> None
Format
Books / Online
8.
Introductory aerodynamics and hydrodynamics of wings and bodies a software-based approach
Author
Smetana, Frederick O., 1928-
Published
Reston, Va. : American Institute of Aeronautics and Astronautics, c1997.
Online
Online book
Location
Yale Internet Resource >> None
Format
Books / Online
9.
Experimental study of lift-enhancing tabs on a two-element airfoil
Author
Storms, Bruce L.
Published
[Washington, D.C.] : [National Aeronautics and Space Administration], [1998]
Online
https://purl.fdlp.gov/GPO/gpo177673
Location
Yale Internet Resource >> None
Format
Books / Online
10.
Combined experiment. Phase I final report
Author
Butterfield, C. P. (Charles P.)
Published
Golden, Colo. : National Renewable Energy Laboratory, [1992]
Online
http://purl.access.gpo.gov/GPO/LPS120571
Location
Yale Internet Resource >> None
Format
Books / Online
11.
The NASA Langley laminar-flow-control experiment on a swept, supercritical airfoil suction coefficient analysis
Author
Brooks, Cuyler W.
Published
[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.
Online
http://purl.access.gpo.gov/GPO/LPS66394
Location
Yale Internet Resource >> None
Format
Books / Online / Microforms
12.
An aerodynamic tradeoff study of the scissor wing configuration
Author
Selberg, Bruce P.
Published
Rolla, Mo. : University of Missouri-Rolla ; [Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, Va. : National Technical Information Service, distributor, 1990]
Online
http://purl.access.gpo.gov/GPO/LPS63191
Location
Yale Internet Resource
Format
Books / Online / Microforms
13.
Wing theory
Author
Jones, Robert T. (Robert Thomas), 1910-1999
Published
Princeton, New Jersey : Princeton University Press, [1990]
©1990
Online
Online book
Location
Yale Internet Resource >> None
Format
Books / Online
14.
Low-speed wind-tunnel results for symmetrical NASA LS(1)-0013 airfoil
Author
Ferris, James C.
Published
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, August 1987.
Online
http://purl.fdlp.gov/GPO/gpo76160
Location
Yale Internet Resource >> None
Format
Books / Online
15.
R4 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel
Author
Jenkins, Renaldo V.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, May 1986.
Online
https://purl.fdlp.gov/GPO/gpo105897
Location
Yale Internet Resource >> None
Format
Books / Online
16.
Critical evaluation of the unsteady aerodynamics approach to dynamic stability at high angles of attack : final report
Author
Hui, W. H.
Published
[Washington, D.C.] : [National Aeronautics and Space Administration], 1985.
Online
https://purl.fdlp.gov/GPO/gpo153324
Location
Yale Internet Resource >> None
Format
Books / Online
17.
Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions
Author
Florschuetz, L. W.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1981.
Online
http://purl.fdlp.gov/GPO/gpo65307
Location
Yale Internet Resource >> None
Format
Books / Online
18.
Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90
Author
Noonan, Kevin W.
Published
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, September 1980.
Online
http://purl.fdlp.gov/GPO/gpo71094
Location
Yale Internet Resource >> None
Format
Books / Online
19.
A rapid implicit-explicit solution to the two-dimensional time-dependent incompressible Navier-Stokes equations
Author
Davis, Joseph E. (Joseph Eugene), 1946-
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980.
Online
http://purl.fdlp.gov/GPO/gpo65128
Location
Yale Internet Resource >> None
Format
Books / Online
20.
Basic wing and airfoil theory
Author
Pope, Alan, 1913-
Published
Mineola, N.Y. : Dover Publications, 2009.
Online
Online book
Location
Yale Internet Resource >> None
Format
Books / Online