Hybrid state vector methods for structural dynamic and aeroelastic boundary value problems
By: Larry Lee Lehman ; prepared for Langley Research Center under grant NGL-05-020-243.
Contributors: Langley Research Center.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.; Stanford University. Dept. of Aeronautics and Astronautics.
Series: NASA contractor report -- 3591.; NASA contractor report -- NASA CR-3591.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1982
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 181
Subjects: Aeroelasticity.; Boundary value problems.; Vector analysis.; Structural dynamics.
Notes: "Stanford University, Dept. of Aeronautics and Astronautics"--Tech. rep. p.

"August 1982"--Cover.

Includes bibliographical references.