Research Catalog
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Displaying 1-18 of 18 results
Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2 [microform] / D. R. Boldman ... [et al.].
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1991]
- 1991
Background noise levels measured in the NASA Lewis 9-by 15-foot low-speed wind tunnel [microform] / Richard P. Woodward ... [et al.].
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Vapor generator wand [microform] / inventor, David B. Robelen.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1994]
- 1994
Low Reynolds number boundary layers in a disturbed environment [microform] / Dong-Kee Paik and Eli Reshotko.
- Text
- [Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1986]
- 1986
Flow quality improvements in the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel [microform] / E. Allen Arrington and Jose C. Gonsalez.
- Text
- [Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test) [microform] / E. Allen Arrington and Jose C. Gonsalez.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Calibration of NASA Lewis Research Center 9- by 15-Foot low speed wind tunnel (1992 text) [microform] / E. Allen Arrington, and Mark T. Pickett and Ronald H. Soeder.
- Text
- [Washington, DC] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Laser velocimetry in the low-speed wind tunnels at Ames Research Center [microform] / Kenneth L. Orloff, Philip K. Snyder, and Michael S. Reinath.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1984]
- 1984
Contraction design for small low-speed wind tunnels / by James H. Bell and Rabindra D. Mehta.
- Text
- [Moffett Field, Calif.?] : National Aeronautics and Space Administration, Ames Research Center ; Stanford, CA : Stanford University, Joint Institute for Aeronautics and Acoustics, [1988]
- 1988
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS112064Contraction design for small low-speed wind tunnels [microform] / by James H. Bell and Rabindra D. Mehta.
- Text
- [Moffett Field, Calif.?] : National Aeronautics and Space Administration, Ames Research Center ; Stanford, CA : Stanford University, Joint Institute for Aeronautics and Acoustics, [1988]
- 1988
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS112064Initial investigation of the acoustics of a counter-rotating open rotor model with historical baseline blades in a low-speed wind tunnel / David M. Elliott.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo26275Acoustic performance of an advanced model turbofan in three aeroacoustic test facilities / Richard P. Woodward and Christopher E. Hughes.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo32152The effect of bypass nozzle exit area on fan aerodynamic performance and noise in a model turbofan simulator / Christopher E. Hughes [and three others].
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 2013.
- 2013-12
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo50531Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / Christopher E. Hughes, John A. Gazzaniga.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Langley Research Center, November 2013.
- 2013-11
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo50535CFD simulations for the effect of unsteady wakes on the boundary layer of a highly loaded low-pressure turbine airfoil (L1A), final report / Samuel J. Vinci.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, September 2012.
- 2012-9
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo33342Modifications to the 4 x 7 meter tunnel for acoustic research : engineering feasibility study.
- Text
- Orlando, Fla. : DSMA Engineering Corporation ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
- 1986
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo28951Quiet High Speed Fan II (QHSF II) : final report / Karen Kontos, Don Weir, and Dave Ross.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, 2012.
- 2012
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo32517Wake characteristics of an eight-leg tower for a MOD-0 type wind turbine / Joseph M. Savino, Lee H. Wagner, and Donald M. Sinclair.
- Text
- Washington, D.C. : National Aeronautics and Space Administration, December 1977.
- 1977-12
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/gpo171498
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