Analysis of a Shock-Associated Noise Prediction Model Using Measured Jet Far-Field Noise Data (AIAA 2014-0176)
52nd, Aerospace sciences meeting; held at the AIAA SciTech Forum 2014 ; 2014 ; National Harbor, MD
2014-01-01
23 pages
Includes bibliographical references and author index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DESIGN AND TESTING OF A SPACE DEPLOYABLE MECHANISM (AIAA 2017-0176)
British Library Conference Proceedings | 2017
|An Enhanced Modal Approach for Large Deformation Modeling of Wing-Like Structures (AIAA 2015-0176)
British Library Conference Proceedings | 2015
|Recurrence Analysis of Combustion Generated Noise (AIAA 2014-0623)
British Library Conference Proceedings | 2014
|British Library Conference Proceedings | 2006
|A Low-order Jet Noise Prediction Model for Chevrons and Microjets (AIAA 2014-0526)
British Library Conference Proceedings | 2014
|