Lateral stability analysis for X-29A drop model using system identification methodology [microform] / David L. Raney and James G. Batterson.

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Bibliographic Details
Main Author:	Raney, David L.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors:	Batterson, James G.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1989.
Series:	NASA technical memorandum ; 4108.
Subjects:	Grumman X-29A (Research plane) Stability of airplanes, Lateral > Measurement. Aircraft models. Directional stability. Drop tests. Flight characteristics. Flight stability tests. Lateral stability. Swept forward wings. System identification. X-29 aircraft.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:4108
NAS 1.15:4108	Restricted Place a Hold