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Displaying 1-6 of 6 results
Limiting vibration in systems with constant amplitude actuators through command preshaping [microform] / by Keith Eric Rogers.
- Text
- Cambridge, Mass. : Charles Stark Draper Laboratory, Inc. ; [Washington, DC : National Aeronautics and Space Administration, 1994]
- 1994
Sloshing of cryogenic helium driven by lateral impulse/gravity gradient-dominated/or g-jitter-dominated accelerations and orbital dynamics [microform] / R.J. Hung, Y.T. Long, and G.J. Zu.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1996]
- 1996
Identification of linear and nonlinear aerodynamic impulse responses using digital filter techniques [microform] / Walter A. Silva.
- Text
- [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1997]
- 1997
Model helicopter rotor high-speed impulsive noise [microform] : measured acoustics and blade pressures / D. A. Boxwell ... [et al.].
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center, [1983]
- 1983
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS89480Helicopter impulsive noise [microform] : theoretical and experimental status / F.H. Schmitz and Y.H. Yu.
- Text
- Moffett Field, Calif. : National Aeronautics and Space Administration, Ames Research Center ; St. Louis, Mo. : United States Army Aviation Research and Development Command, [1983]
- 1983
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS99773Multiple-cycle simulation of a pulse detonation engine ejector / S. Yungster, H.D. Perkins.
- Text
- Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, October 2002.
- 2002-10
- 1 Resource
Available Online
https://purl.fdlp.gov/GPO/LPS53266
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