Research Catalog
New! Try our Article Search to discover online journals, books, and more from home with your library card.
Displaying 1-30 of 30 results
Navier-Stokes simulation of several high-lift reference H configurations [microform] / Wendy B. Lessard.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover, MD : Available from NASA Center for AeroSpace Information ; Springfield, VA : National Technical Information Service [distributor, 1999]
- 1999
1999 NASA High-Speed Research Program Aerodynamic Performance Workshop [microform] : proceedings of a workshop sponsored by the National Aeronautics and Space Administration, Washington D.C., and held in Anaheim, California, February 8-12, 1999 / edited by David E. Hahne.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999- ]
- 1999-present
Integrated design and manufacturing for the high speed civil transport [microform] : preliminary design methodology and optimization for an HSCT Nacelle/Wing configuration : final report.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Cabin-fuselage-wing structural design concept with engine installation [microform].
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
HOMAR:a computer code for generating homotopic grids using algebraic relations [microform] : users' manual / Anutosh Moitra.
- Text
- [Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : National Technical Information Service, distributor], 1989.
- 1989
Development of direct-inverse 3-D method for applied aerodynamic design and analysis [microform] : semiannual progress report, July 1, 1986 - December 31, 1986 / Leland A. Carlson.
- Text
- College Station, Tex. : Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1987]
- 1987
Aerodynamic shape optimization of wing and wing-body configurations using control theory [microform] / James Reuther and Antony Jameson.
- Text
- [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Aeroelasticity of wing and wing-body configurations on parallel computers [microform] / Chansup Byun.
- Text
- San Jose, CA : MCAT Institute ; [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept [microform] / A.M. Springer.
- Text
- MSFC, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Supersonic wing and wing-body shape optimization using an adjoint formulation [microform] / James Reuther and Antony Jameson.
- Text
- [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Parallel aeroelastic computations for wing and wing-body configurations [microform] : annual report for the period of time July 1993-July 1994 / Chansup Byun.
- Text
- San Jose, CA : MCAT Institute ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Wing weight optimization under aeroelastic loads subject to stress constraints [microform] / Rakesh K. Kapania ... [et al.].
- Text
- [Washington, DC : National Aeronautics and Space Administration, 1997]
- 1997
Aerodynamic shape optimization of complex aircraft configurations via an adjoint formulation [microform] / James Reuther ... [et al.].
- Text
- [Moffett Field, Calif.] : Research Institute for Advanced Computer Science, NASA Ames Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Development of multiobjective optimization techniques for sonic boom minimization [microform] : final report on NASA Ames grant no. NCC2-5064, performance period--5/16/94-9/15/96 / principal investigators: Aditi Chattopadhyay and John Narayan Rajadas, Narayanan S. Pagaldipti.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Wing-body aeroelasticity on parallel computers [microform] / Chansup Byun and Guru P. Guruswamy.
- Text
- Washington, DC : American Institute of Aeronautics and Astronautics : [National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Study of the mutual interaction between a wing wake and an encountering airplane [microform] : NASA grant no. NAG1-1572, final report / by A.B. Walden, C.P. van Dam.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results [microform] / Jim A. Penland and Richard Hawkins.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Springfield, VA : National Technical Information Service, distributor, [1997]
- 1997
Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds [microform] / Robert J. Mack.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1999]
- 1999
Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D [microform] / Christopher L. Rumsey and Robert T. Biedron.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; Hanover MD : Available from NASA Center for AeroSpace Information (CASI), [2001]
- 2001
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS27157Effects of upper-surface nacelles on longitudinal aerodynamic characteristics of high-wing transport configuration [microform] / Lawrence E. Putnam.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1986.
- 1986
Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations [microform] / Gregory M. Gatlin.
- 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/LPS68634Unsteady transonic flow calculations for wing-fuselage configurations [microform] / John T. Batina.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
- 1986
Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds [microform] / M. Leroy Spearman.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
- 1986
Comparison of computational results of a few representative three-dimensional transonic potential flow analysis programs [microform] / Tanaka, K. and Hirose, H.
- Text
- Washington, D.C. : National Aeronautics and Space Administration, [1986]
- 1986
Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model / Raymond Castner, Troy Lake.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo30596PRSEUS panel fabrication final report / Kim A. Linton [and five others].
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, January 2014.
- 2014-1
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo52596Modal filtering for control of flexible aircraft / Peter M. Suh, Dimitri N. Mavris.
- Text
- Edwards, CA : National Aeronautics and Space Administration, Dryden Flight Research Center, September 2013.
- 2013-9
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo54680Enabling rapid and robust structural analysis during conceptual design / Lloyd B. Eldred, Sharon L. Padula, and Wu Li.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, February 2015.
- 2015-2
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo57878Compressive testing of stitched frame and stringer alternate configurations / Frank A. Leone, Jr., Dawn C. Jegley.
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, April 2016.
- 2016-4
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo69164Performance evaluation of speech recognition systems as a next-generation pilot-vehicle interface technology / Jarvis (Trey) J. Arthur III [and three others].
- Text
- Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, August 2016.
- 2016-8
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo71794
No results found from Digital Research Books Beta
Digital books for research from multiple sources world wide- all free to read, download, and keep. No Library Card is Required. Read more about the project.
