Propulsion System Integration Effects on Mixer-ejector Nozzle Acoustics and Exhaust Flow PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Propulsion System Integration Effects on Mixer-ejector Nozzle Acoustics and Exhaust Flow PDF full book. Access full book title Propulsion System Integration Effects on Mixer-ejector Nozzle Acoustics and Exhaust Flow by Naseem H. Saiyed. Download full books in PDF and EPUB format.
Author: Naseem H. Saiyed
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author: Naseem H. Saiyed
Publisher:
ISBN:
Category :
Languages : en
Pages :
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 636
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 920
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 630
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 384
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 352
Get Book Here
Book Description
Author: Aaron J. Glaser
Publisher:
ISBN:
Category :
Languages : en
Pages : 241
Get Book Here
Book Description
The acoustic signature of a pulse detonation engine was characterized in both the near-field and far-field regimes. Experimental measurements were performed in an anechoic test facility designed for jet noise testing. Both shock strength and speed were mapped as a function of radial distance and direction from the PDE exhaust plane. It was found that the PDE generated pressure field can be reasonably modeled by a theoretical point-source explosion. The effect of several exit nozzle configurations on the PDE acoustic signature was studies. These included various chevron nozzles, a perforated nozzle, and a set of proprietary noise attenuation mufflers.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1048
Get Book Here
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
