Lateral stability analysis for X-29A drop model using system identification methodology
By: David L. Raney and James G. Batterson.
Contributors: Batterson, James G.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4108.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; For sale by the National Technical Information Service]
Published: 1989
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 24
Subjects: Grumman X-29A (Jet 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.
Notes: Distributed to depository libraries in microfiche.

Includes bibliographical references (p. 7).

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1989] 1 microfiche : negative.