Research Catalog
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Displaying 1-5 of 5 results
Lateral stability analysis for X-29A drop model using system identification methodology [microform] / David L. Raney and James G. Batterson.
- Text
- [Washington, DC] : 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
Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50̊ [microform] / Scott P. Fears, Holly M. Ross, and Thomas M. Moul.
- Text
- [Washington, DC : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1995]
- 1995
Estimation of aircraft nonlinear unsteady parameters from wind tunnel data [microform] / Vladislav Klein, Patrick C. Murphy.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center ; [Springfield, Va. : National Technical Information Service, distributor, 1998]
- 1998
Final design proposal [microform] : the MANTA : an RPV designed to investigate forces and moments on a lifting surface / [Kevin Bryan ... et al.].
- Text
- Notre Dame, IN : Dept. of Aerospace and Mechanical Engineering, University of Notre Dame ; [Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, distributor, 1990]
- 1990
- 1 Resource
Available Online
http://purl.access.gpo.gov/GPO/LPS63197Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data [microform] / William T. Suit and James G. Batterson.
- Text
- Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1986]
- 1986
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