Response of multi-panel assembly to noise from a jet in forward motion
By: A. Bayliss ... [et al.].
Contributors: Bayliss, Alvin.; Institute for Computer Applications in Science and Engineering.
Series: ICASE report -- no. 95-41.; NASA contractor report -- 198164.; NASA contractor report -- NASA CR-198164.
Publisher: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, VA; [Springfield, Va
Language: eng
Format: Microform
Subjects: Aeroacoustics.; Aerodynamic noise.; Boundary layer flow.; Jet aircraft noise.; Jet flow.; Noise prediction.; Panels.; Shock wave interaction.; Subsonic flow.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0750-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.