Experimental flutter boundaries with unsteady pressure distributions for the NACA 0012 Benchmark Model
By: José A. Rivera ... [et al.].
Contributors: Rivera, José A.; Langley Research Center.
Series: NASA technical memorandum -- 104072.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1991
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aeroelasticity.; Airfoil dynamics.; Flutter analysis.; Pressure distribution.; Unsteady flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 92-0349-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1991] 1 microfiche.