Explore: Conical Nozzles
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1A performance comparison of two small rocket nozzles
By Lynn A. Arrington
“A performance comparison of two small rocket nozzles” Metadata:
- Title: ➤ A performance comparison of two small rocket nozzles
- Author: Lynn A. Arrington
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“A performance comparison of two small rocket nozzles” Subjects and Themes:
- Subjects: ➤ Rocket thrust - Thrust chamber pressure - Nozzle design - Reynolds number - Rocket nozzles - Conical nozzles - Film cooling
Edition Identifiers:
- The Open Library ID: OL15452208M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
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2Computational noise study of a supersonic short conical plug-nozzle jet
By Indu S. Das
“Computational noise study of a supersonic short conical plug-nozzle jet” Metadata:
- Title: ➤ Computational noise study of a supersonic short conical plug-nozzle jet
- Author: Indu S. Das
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics & Space Administration
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Computational noise study of a supersonic short conical plug-nozzle jet” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Pressure ratio - Supersonic nozzles - Plug nozzles - Conical nozzles - Aerodynamic noise - Noise reduction - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL15548349M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Computational noise study of a supersonic short conical plug-nozzle jet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Thrust coefficient
}}{2}}\right)} α {\displaystyle \alpha } is the half-angle of the conical nozzle (rad) These nozzles are typically found in aerospike engines or in jet engines
Aerospike engine
The term aerospike was originally used for a truncated plug nozzle with a rough conical taper and some gas injection, forming an "air spike" to help
Vortex tube
vortex—as it moves along the inner surface of the tube to the far end. A conical nozzle allows gas specifically from this outer layer to escape at that end
Conical plate centrifuge
through nozzles continuously, as shown in Figure 2[clarification needed]. The quantity of concentrate depends on speed of bowl rotation, number of nozzles per
Bell nozzle
extremes of the conical nozzle since it minimizes weight while maximizing performance. The most important design issue is to contour the nozzle to avoid oblique
Enema
injecting the smoke using a rectal tube. A rubber bag connected with a conical nozzle, at an early period, was in use among the indigenous peoples of South
Plug nozzle
hose trigger nozzles are a simple example of the plug nozzle and its method of operation. In this example the nozzle consists of a conical or bell shaped
Vortex ring
This is referred as a parallel starting jet. It is possible to have a conical nozzle in which the streamlines at the exhaust are directed toward the centerline
Components of jet engines
feature two conical surfaces: the first cone is supplemented by a second, less oblique, conical surface, which generates an extra conical shockwave, radiating
Aerodynamic levitation
spherical samples to be levitated by passing gas up through a diverging conical nozzle. Combining this with >200W continuous CO2 laser heating allows sample