Acoustic and laser doppler anemometer results for confluent, 22-lobed, and unique-lobed mixer exhaust systems for subsonic jet noise reduction

Acoustic and laser doppler anemometer results for confluent, 22-lobed, and unique-lobed mixer exhaust systems for subsonic jet noise reduction

Show other versions (2)
Saved in:
Bibliographic Details
Corporate Author: NASA Glenn Research Center
Other Authors: Salikuddin, M
Format: Government Document Book
Language:English
Published: [Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, [2002]
Series:NASA contractor report NASA CR-211598
Subjects:
Acoustics
Aerodynamic noise
Engine design
Exhaust systems
Jet aircraft noise
Laser anemometers
Laser doppler velocimeters
Noise reduction
Tags: Add Tag
No Tags, Be the first to tag this record!

Internet

This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.

Stanford University

Holdings details from Stanford University
Call Number: NAS 1.26:2002-211598

Similar Items