0

Performance Analysis of Plug Nozzles for Turbojet and Rocket Exhausts FREE

[+] Author Affiliations
W. H. Krase

The Rand Corporation, Santa Monica, CA

Paper No. 59-GTP-9, pp. V001T01A009; 8 pages
doi:10.1115/59-GTP-9
From:
  • ASME 1959 Gas Turbine Power Conference and Exhibit
  • ASME 1959 Gas Turbine Power Conference and Exhibit
  • Cincinnati, Ohio, USA, March 8–11, 1959
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7996-2
  • Copyright © 1959 by ASME

abstract

An attractive feature of the plug-type nozzle for turbojets and rocket jets is that it can automatically adjust its effective exit area with operating pressure ratio and achieve a high level of efficiency over a wide range of operating pressure ratio without variation of mechanical shape. The design and off-design performance analysis of such nozzles is described.

Copyright © 1959 by ASME
Topics: Nozzles , Rockets , Turbojets
This article is only available in the PDF format.

Figures

Tables

Interactive Graphics

Video

Country-Specific Mortality and Growth Failure in Infancy and Yound Children and Association With Material Stature

Use interactive graphics and maps to view and sort country-specific infant and early dhildhood mortality and growth failure data and their association with maternal

NOTE:
Citing articles are presented as examples only. In non-demo SCM6 implementation, integration with CrossRef’s "Cited By" API will populate this tab (http://www.crossref.org/citedby.html).

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In