Acoustic and aerothermal performance test of the axisymmetric coannular ejector nozzle
By: William Herkes.
Contributors: NASA Glenn Research Center.
Series: [NASA contractor report] -- NASA CR-2000-209813.; NASA contractor report -- NASA CR-209813.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for AeroSpace Information; National Technical Information Service [distributor
Published: 2000
Place of publication: [Cleveland, Ohio]; Hanover, MD; Springfield, VA
Language: eng
Format: Microform
Subjects: Jet nozzles -- Noise.; Jet planes -- Noise.; Acoustic properties.; Aeroacoustics.; Effective perceived noise levels.; Noise reduction.; Performance tests.; Plug nozzles.; Ejectors.; Aerodynamic noise.; Jet aircraft noise.; Wind tunnel tests.
Notes: Shipping list no.: 2000-0583-M (v. 2).

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2000- <2> microfiches.
Table of contents: title: v. 2. Acoustic performance.