Loads model development and analysis for the F/A-18 Active Aeroelastic Wing airplane /

Bibliographic Details

Corporate Author:	Hugh L. Dryden Flight Research Center
Other Authors:	Allen, Michael J.
Format:	Government Document eBook
Language:	English
Published:	Edwards, Calif. : National Aeronautics and Space Administration, Dryden Flight Research Center, [2005]
Series:	NASA technical memorandum ; 213663.
Subjects:	Loads (Forces) F-18 aircraft. Aeroelastic research wings. Mathematical models.
Online Access:	https://purl.fdlp.gov/GPO/gpo2033