Research Catalog
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Displaying 1-16 of 16 results
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
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
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
Cryogenic tunnel pressure measurements on a supercritical airfoil for several shock buffet conditions [microform] / Robert E. Bartels and John W. Edwards.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails [microform] : 36th Aerospace Sciences meeting & exhibit : January 12-15, 1998/Reno, NV / Robert W. Moses, Holt Ashley.
- Text
- Reston, Va. : American Institute of Aeronautics and Astronautics ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications [microform] : final report for the period December 1, 1995 through Novemeber 30, 1996 / principal investigator, Osama A. Kandil ; submitted by the Old Dominion University Research Foundation.
- Text
- Norfolk, Va. : Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
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
Aerostructural vortical flow interactions with applications to F/A-18 and F-117 tail buffet [microform] / Osama A. Kandil, Steven J. Massey and Essam F. Sheta.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Flow and turbulence modeling and computation of shock buffet onset for conventional and supercritical airfoils [microform] / Robert E. Bartels.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1998]
- 1998
Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances [microform] / Lisa J. Bjarke.
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Facility ; [Springfield, Va. : National Technical Information Service, distributor, 1990]
- 1990
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS59777Dynamic response of a hammerhead launch vehicle wind-tunnel model [microform] / Stanley R. Cole, Thomas L. Henning.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1991]
- 1991
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS64065Experimental verification of buffet calculation procedure using unsteady PSP / Jayanta Panda.
- Text
- Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, February 2016.
- 2016-2
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo67582Assessment of JVX proprotor performance data in hover and airplane-mode flight conditions / C.W. Acree, Jr.
- Text
- Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, February 2016.
- 2016-2
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo68686Vertical 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/LPS60727Effect of canard position and wing leading-edge flap deflection on wing buffet at transonic speeds / by Blair B. Gloss, William P. Henderson, and Jarrett K. Huffman.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 1975.
- 1975-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo157696Some aspects of aircraft dynamic loads due to flow separation / by D.G. Mabey.
- Text
- Neuilly-sur-Seine, France : AGARD, 1988.
- 1988
- 1 Item
Item details Format Call Number Item Location Text AGARD-R-750 Off-site
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