Effect of speed (centrifugal load) on gear crack propagation directionFormat: [microform] /
Author: Lewicki, David G.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: [2001] This title can be found in 1 Iowa libraries.
Numerical speed of sound and its application to schemes for all speedsFormat: [microform] /
Author: Liou, M. S.
Publisher: [Cleveland, Ohio] : National Aeronautics and Space Administration, Glenn Research Center ;
Date: 1999] This title can be found in 2 Iowa libraries.
Low-speed stability-and-control and ground-effects measurements on the industry reference high speed civil transportFormat: [microform] /
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1999] This title can be found in 1 Iowa libraries.
Low speed analysis of mission adaptive flaps on a high speed civil transport configurationFormat: [microform] /
Author: Lessard, Victor R.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: [1999] This title can be found in 2 Iowa libraries.
Low speed aerodynamics of the X-38 CRV summary of research NAG9-927, 5/97-4/98 /Format: [microform] :
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1998] This title can be found in 2 Iowa libraries.
Calibration of the NASA Lewis Research Center 9- by 15-foot low speed wind tunnel (1994 test)Format: [microform] /
Author: Arrington, E. Allen.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
Effects of stator indexing on performance in a low speed multistage axial compressorFormat: [microform] /
Author: Barankiewicz, Wendy S.
Publisher: [Washington, D.C. : National Aeronautics and Space Administration ;
Date: 1997] This title can be found in 2 Iowa libraries.
Planetary and primitive object strength measurements and sampling apparatus NASA #NAGW 2439, final report; February 1, 1991 through January 31, 1997 /Format: [microform] :
Author: Ahrens, T. J.
Publisher: Pasadena, Calif. : California Institute of Technology, Seismological Laboratory ;
Date: 1997] This title can be found in 2 Iowa libraries.
Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider conceptFormat: [microform] /
Author: Hahne, David E.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1997] This title can be found in 2 Iowa libraries.
Preconditioning methods for low-speed flowsFormat: [microform] /
Author: Turkel, E.
Publisher: Hampton, VA : Institute for Computer Applications in Science and Engineering, NASA Langley Research Center ;
Date: 1996] This title can be found in 2 Iowa libraries.
A survey of Reynolds number and wing geometry effects on lift characteristics in the low speed stall regionFormat: [microform] /
Author: Polhamus, Edward C.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1996] This title can be found in 2 Iowa libraries.
Calibration of NASA Lewis Research Center 9- by 15-Foot low speed wind tunnel (1992 text)Format: [microform] /
Author: Aarington, E. Allen.
Publisher: [Washington, DC] : National Aeronautics and Space Administration ;
Date: 1996] This title can be found in 2 Iowa libraries.
NASA low-speed axial compressor for fundamental researchFormat: [microform] /
Author: Wasserbauer, Charles A.
Publisher: [Springfield, Va. : National Technical Information Service, distributor], [Springfield, Va. : National Technical Information Service, distributor],
Date: 1995. This title can be found in 2 Iowa libraries.
NASA low-speed axial compressor for fundamental researchFormat: [microform] /
Author: Wasserbauer, Charles A.
Publisher: [Springfield, Va. : National Technical Information Service, distributor], [Springfield, Va. : National Technical Information Service, distributor],
Date: 1995. This title can be found in 1 Iowa libraries.
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50Format: [microform] /
Author: Fears, Scott P.
Publisher: [Washington, DC : National Aeronautics and Space Administration ;
Date: 1995] This title can be found in 2 Iowa libraries.
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 70 /Author: Ross, Holly M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1995] This title can be found in 1 Iowa libraries.
Evaluation of the impact response of textile compositesFormat: [microform] /
Author: Portanova, M. A.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1995] This title can be found in 2 Iowa libraries.
Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapesFormat: [microform] /
Author: Catlin, Gregory M.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: 1995] This title can be found in 2 Iowa libraries.
Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2 /Publisher: [Washington, D.C.] : National Aeronautics and Space Administration,
Date: [1991] This title can be found in 1 Iowa libraries.
Response of composite materials to low velocity impact /Author: Srinivasan, K.
Publisher: Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ;
Date: [1991] This title can be found in 1 Iowa libraries.
This resource is supported by the Institute of Museum and Library Services under the provisions of the Library Services and Technology Act as administered by State Library of Iowa.