Explore: Supersonic Turbines
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance
By Nateri K. Madavan
“Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance” Metadata:
- Title: ➤ Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance
- Author: Nateri K. Madavan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Neural net-based redesign of transonic turbines for improved unsteady aerodynamic performance” Subjects and Themes:
- Subjects: Supersonic turbines - Design analysis - Fluid dynamics - Navier-Stokes equation - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17839330M - OL18134349M - OL15546637M - OL17131903M
- Online Computer Library Center (OCLC) ID: 41598306
Access and General Info:
- First Year Published: 1998
- 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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2Unsteady blade row interaction in a transonic turbine
By Daniel J. Dorney
“Unsteady blade row interaction in a transonic turbine” Metadata:
- Title: ➤ Unsteady blade row interaction in a transonic turbine
- Author: Daniel J. Dorney
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Unsteady blade row interaction in a transonic turbine” Subjects and Themes:
- Subjects: ➤ Engine tests - Supersonic turbines - Jet engines - Unsteady flow - Three dimensional flow - Turbomachinery
Edition Identifiers:
- The Open Library ID: OL17837381M - OL15506834M
- Online Computer Library Center (OCLC) ID: 40115463
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
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3Turbomachinery design and tonal acoustics computations
By Akil A. Rangwalla
“Turbomachinery design and tonal acoustics computations” Metadata:
- Title: ➤ Turbomachinery design and tonal acoustics computations
- Author: Akil A. Rangwalla
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - MCAT Institute
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va - San Jose, CA
“Turbomachinery design and tonal acoustics computations” Subjects and Themes:
- Subjects: ➤ Supersonic turbines - Unsteady flow - Computer aided design - Secondary flow - Aeroacoustics - Three dimensional flow
Edition Identifiers:
- The Open Library ID: OL15413738M
Access and General Info:
- First Year Published: 1995
- 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.
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4Supersonic through-flow fan engine and aircrraft mission performance
By Leo C. Franciscus
“Supersonic through-flow fan engine and aircrraft mission performance” Metadata:
- Title: ➤ Supersonic through-flow fan engine and aircrraft mission performance
- Author: Leo C. Franciscus
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - For sale by the National Technical Information Service
- Publish Date: 1989
- Publish Location: ➤ Springfield, Va - [Cleveland, Ohio
“Supersonic through-flow fan engine and aircrraft mission performance” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Engine design - Supersonic planes - Turbines - Supersonic turbines - Turbofan engines - Aerodynamics - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL16128767M
Access and General Info:
- First Year Published: 1989
- 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
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5Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade
By Tony Arts
“Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade” Metadata:
- Title: ➤ Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade
- Author: Tony Arts
- Publisher: ➤ von Karman Institute for Fluid Dynamics
- Publish Date: 1990
- Publish Location: Rhode Saint Genese, Belgium
“Aero-thermal investigation of a highly loaded transonic linear turbine guide vane cascade” Subjects and Themes:
- Subjects: Supersonic turbines
Edition Identifiers:
- The Open Library ID: OL21335292M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
De Laval nozzle
nozzles are widely used in some types of steam turbines and rocket engine nozzles. It also sees use in supersonic jet engines. Similar flow properties have
Gas turbine
such as micro turbines and also have strong potential for use in small gas turbines/auxiliary power units A major challenge facing turbine design, especially
Turbojet
the combustor expand through the turbine. Typical materials for turbines include inconel and Nimonic. The hottest turbine vanes and blades in an engine have
Scramjet
A scramjet (supersonic combustion ramjet) is a variant of a ramjet airbreathing jet engine in which combustion takes place in supersonic airflow. As in
Afterburner
jet engines, mostly those on military supersonic aircraft. Its purpose is to increase thrust, usually for supersonic flight, takeoff, and combat. The afterburning
Supersonic transport
A supersonic transport (SST) or a supersonic airliner is a civilian supersonic aircraft designed to transport passengers at speeds greater than the speed
Components of jet engines
rotating at independent speeds, with as many sets of turbines and compressors. Cooling air for the turbines may flow through the shaft from the compressor.
Variable cycle engine
such as subsonic, transonic and supersonic. An advanced technology engine is a turbine engine that allows different turbines to spin at different, individually
Supersonic aircraft
A supersonic aircraft is an aircraft capable of supersonic flight, that is, flying faster than the speed of sound (Mach 1). Supersonic aircraft were developed
Boom Technology
Boom Technology, Inc. (trade name Boom Supersonic) is an American company developing the Overture, a supersonic airliner. It has also flight tested a one-third-scale