X-29A lateral-directional stability and control derivatives extracted from high-angle-of-attack flight data
By: Kenneth W. Iliff, Kon-Sheng Charles Wang.
Contributors: Wang, Kon-Sheng Charles.; Hugh L. Dryden Flight Research Center.
Series: NASA technical paper -- 3664
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program Center
Published: 1996
Place of publication: [Washington, D.C]
Language: eng
Number of pages: 35
Subjects: Airplanes -- Control systems.; Angle of attack (Aerodynamics); Grumman X-29A (Jet plane); Research aircraft.; Stability of airplanes, Lateral.; Yawing (Aerodynamics)
Notes: "December 1996."

"Performing organization report number H-2118"--Report documentation page.

Includes bibliographical references.

Performed by NASA Dryden Flight Research Center for the National Aeronautics and Space Administration WU 505 68 50 00R