Research Catalog
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Displaying 1-28 of 28 results
Modeling of longitudinal unsteady aerodynamics of a wing-tail combination [microform] / Vladislav Klein.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Low speed analysis of mission adaptive flaps on a high speed civil transport configuration [microform] / Victor R. Lessard.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1999]
- 1999
A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept [microform] / Bandu N. Pamadi.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
An experimental study of the aerodynamics of a NACA0012 airfoil with a simulated glaze ice accretion. Volume II [microform] / Mike A. Bragg.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
- 1993
Development of a mulicomponent force and moment balance for water tunnel applications [microform] / Carlos J. Suárez ... [et al.].
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; [Springfield, Va. : National Technical Information Service, distributor], 1994.
- 1994
Effects of yaw and pitch motion on model attitude measurements [microform] / Ping Tcheng, John S. Tripp, and Tom D. Finley.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
An examination of the aerodynamic moment on rotor blade tips using flight test data and analysis [microform] / Thomas H. Maier and William G. Bousman.
- Text
- Moffett Field, Calif. : US Army Aviation and Troop Command : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1993]
- 1993
SOFIA II model telescope and wind tunnel test [microform] / Paul Keas.
- Text
- [Moffett Field, Calif.] : NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept [microform] / B. Spencer, Jr., C.H. Fox, Jr., and J.K. Huffman.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes [microform] / Gregory M. Catlin, Brian E. McGrath.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Low-speed wind tunnel tests of two waverider configuration models [microform] / Robert J. Pegg, David E. Hahne, Charles E. Cockrell, Jr.
- Text
- Washington, D.C. : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Aerodynamic limitations of the UH-60A rotor [microform] / Colin P. Coleman, William G. Bousman.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly [microform] / Gregory J. Brauckmann; John W. Paulson, Jr.; K. James Weilmuenster.
- Text
- Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet [microform] / Richard E. Kuhn.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Assessment of dual-point drag reduction for an executive-jet modified airfoil section [microform] / Dennis O. Allison and Raymond E. Mineck.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Wind-tunnel development of an SR-71 aerospike rocket flight test configuration [microform] / Timothy R. Moes ... [et al.].
- Text
- Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center ; [Springfield, Va. : National Technical Information Service, distributor], 1996.
- 1996
Reducing wind tunnel data requirements using neural networks [microform] / James C. Ross and Charles C. Jorgenson, Magnus Norgaard.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Simulation of a controlled airfoil with jets [microform] / Brian G. Allan, Maurice Holt, and Andrew Packard.
- Text
- Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
- 1997
Hypersonic pitching-moment shift for stardust reentry capsule forebody [microform] / William A. Wood.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
- 1997
Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept [microform] / David E. Hahne.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Study of the TRAC airfoil table computational system [microform] / Hong Hu.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Summary of longitudinal stability and control parameters as determined from space shuttle Challenger flight test data [microform] / William T. Suit.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, VA : For sale by the National Technical Information Service, 1989]
- 1989
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS93085Prediction of wing aeroelastic effects on aircraft lift and pitching moment characteristics [microform] / Clinton V. Eckstrom.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
- 1986
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS101897An exploratory investigation of a slotted, natural-laminar-flow airfoil / Dan M. Somers.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo27796Further evaluation of scaling methods for rotorcraft icing / Jen-Ching Tsao, Richard E. Kreeger.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo30594Analysis of a split-plot experimental design applied to a low-speed wind tunnel investigation / Gary E. Erickson.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2013.
- 2013
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo51536Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept / David E. Hahne.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, May 1997.
- 1997-5
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo65472Hypersonic pitching-moment shift for stardust reentry capsule forebody / William A. Wood.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, October 1997.
- 1997-10
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo212744
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