Kids Library Home

Welcome to the Kids' Library!

Search for books, movies, music, magazines, and more.

     
Available items only
E-Book/E-Doc
Author Dahl, Milo D., 1956- author.

Title The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct / Milo D. Dahl.

Publication Info. Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, November 1996.

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.15:107358    ---  Available
Description 1 online resource (21 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series NASA technical memorandum ; 107358
NASA technical memorandum ; 107358.
Note Title from title screen (viewed Aug. 2, 2016).
"November 1996"--Report documentation page.
"Prepared for the International Mechanical Engineering Congress and Exposition sponsored by the American Society of Mechanical Engineers, Atlanta, Georgia, November 17-22, 1996."
"Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
Bibliography Includes bibliographical references (pages 11-12).
Funding Sponsored by the National Aeronautics and Space Administration WU-505-62-52 E-10513
Subject Supersonic jet flow.
Ducts.
Ducted flow.
Duct geometry.
Circles (Geometry)
Boundary conditions.
Kelvin-Helmholtz instability.
Supersonic inlets.
Genre/Form Online resources.
Electronic books.
Electronic government information.
Added Author Lewis Research Center, issuing body.
United States. National Aeronautics and Space Administration, sponsoring body.
Other Form: Print version: Dahl, Milo D. Effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct (OCoLC)60396633
Microfiche version: Dahl, Milo D., 1956- Effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct (OCoLC)39722385
Gpo Item No. 0830-H-15 (online)
Sudoc No. NAS 1.15:107358

 
    
Available items only