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Program of Research in Flight Dynamics in the JIAFS, George Washington University at NASA Langley Research CenterThe program objectives are fully defined in the original proposal entitled 'Program of Research in Flight Dynamics in GW at NASA Langley Research Center,' which was originated March 20, 1975, and in the renewals of the research program from December 1, 2000 to November 30, 2001. The program in its present form includes three major topics: 1) the improvement of existing methods and development of new methods for wind tunnel and flight test data analysis, 2) the application of these methods to wind tunnel and flight test data obtained from advanced airplanes, 3) the correlation of flight results with wind tunnel measurements, and theoretical predictions. The Principal Investigator of the program is Dr. Vladislav Klein. Three Graduate Research Scholar Assistants (K. G. Mas, M. M. Eissa and N. M. Szyba) also participated in the program. Specific developments in the program during the period Dec. 1, 2001 through Nov. 30, 2002 included: 1) Data analysis of highly swept delta wing aircraft from wind and water tunnel data, and 2) Aerodynamic characteristics of the radio control aircraft from flight test.
Document ID
20030015759
Acquisition Source
Langley Research Center
Document Type
Contractor or Grantee Report
Authors
Klein, Vladislav (George Washington Univ. Washington, DC United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2002
Subject Category
Aircraft Stability And Control
Funding Number(s)
CONTRACT_GRANT: NCC1-326
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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