Detailed analysis and test correlation of a stiffened composite wing panel
By: D. Dale Davis, Jr.
Contributors: United States. Army Aviation Research and Technology Activity.; Langley Research Center.
Series: NASA technical memorandum -- 104154.; AVSCOM technical report -- 91-B-015.; AVSCOM technical report -- 91-B-15.
Publisher: National Aeronautics and Space Administration, Langley Research Center; US Army Aviation Systems Command, Aviation R&T Activity
Published: 1991
Place of publication: Hampton, Va; [St. Louis, Mo.]
Language: eng
Format: Microform
Subjects: Finite element method.; Airplanes -- Wings.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-1308-M.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1992. 1 microfiche.