Hybrid residual flexibility/mass-additive method for structural dynamic testing
By: M.L. Tinker.
Contributors: George C. Marshall Space Flight Center.
Series: NASA/TM -- 2003-212343.; NASA technical memorandum -- 212343.
Publisher: National Aeronautics and Space Administration, Marshall Space Flight Center; Available from the NASA Center for Aerospace Information; National Technical Information Service [distributor
Published: 2003
Place of publication: MSFC, Ala; Hanover, MD; Springfield, VA
Language: eng
Format: Microform
Subjects: Test equipment.; Dynamic tests.; Dynamic structural analysis.; Coupled modes.; Design.
Other titles: Hybrid residual flexibility mass additive method for structural dynamic testing.
Notes: Shipping list no.: 2003-0488-M.

"March 2003."

Also available via Internet from the NASA Technical Report Server web site. Address as of 12/21/04:  http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20030032438%5F2003026735.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2003?].