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Viper cabin-fuselage structural design concept with engine installation and wing structural design [microform]
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1993]
1993
0 resources
Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 [microform] / Ira J. Walker, Peter F. Covell And Dana K. Forrest.
Text
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1993.
1993
0 resources
Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model [microform] / Stacey J. Cotton and Lisa J. Bjarke.
Text
Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
1994
0 resources
Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters [microform] / Cynthia A. Crowell and Henry L. Kelley.
Text
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
Some buffet response characteristics of a twin-vertical-tail configuration [microform] / Stanley R. Cole, Steven W. Moss, and Robert V. Doggett.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
1990
0 resources
Flow-field survey of an empennage wake interacting with a pusher propeller [microform] / W. Clifton Horne, Paul T. Soderman.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; Springfield, Va. : For sale by the National Technical Information Service, [1988]
1988
0 resources
Tailless aircraft performance improvements [microform] / Irving L. Ashkenas and David H. Klyde.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1989]
1989
0 resources
Advanced manufacturing development of a composite empennage component for L-1011 aircraft. Phase III, Final report, Production readiness verification testing [microform] / A. Jackson ... [et al.].
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1984]
1984
0 resources
Investigation of empennage buffeting [microform] : technical report CRINC-FRL-714-1 / by C. Edward Lan and I.G. Lee, William H. Wentz.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
1986
0 resources
Numerical simulation of the SOFIA flow field [microform] / Stephen P. Klotz.
Text
San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Aerodynamic characteristics of several current helicopter tail boom cross sections including the effect of spoilers [microform] / John C. Wilson and Henry L. Kelley.
Text
[Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service, distributor], 1986.
1986
0 resources
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊ [microform] / Scott P. Fears, Holly M. Ross, and Thomas M. Moul.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
1995
0 resources
Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail [microform] / by Matthew Robert Whiting.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Development and testing of airfoils for high-altitude aircraft [microform] : final report / principal investigator, Mark Drela.
Text
[Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails [microform] / C. Michael Fremaux.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : For sale by the National Technical Information Service, 1997]
1997
0 resources
A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet [microform] / Robert W. Moses, Ed Pendleton.
Text
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
1996
0 resources
Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes [microform] / James S. Bowman, Jr., Randy S. Hultberg, Colin A. Martin.
Text
[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
1 resource
Available online
http://purl.access.gpo.gov/GPO/LPS68623Wind tunnel acoustic study of a propeller installed behind an airplane empennage [microform] : data report / J. F. WiIby, E. G. Wilby.
Text
Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1985]
1985
0 resources
AFC-enabled vertical tail system integration study / Helen P. Mooney [and three others].
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, March 2014.
2014-3
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo51182Flight services and aircraft access : active flow control vertical tail and insect accretion and mitigation flight test / Edward A. Whalen.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2016.
2016-1
1 resource
Available online
https://purl.fdlp.gov/GPO/gpo72515Vertical tail buffeting alleviation using piezoelectric actuators : some results of the Actively Controlled Response of Buffet-Affected Tails (ACROBAT) program / Robert W. Moses.
Text
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 1997.
1997-4
1 resource
Available online
https://purl.fdlp.gov/GPO/LPS60727No results found from Digital Research Books Beta
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