Explore: Exhaust Flow Simulation
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Hot-jet simulation in cryogenic wind tunnels
By Keisuke Asai
“Hot-jet simulation in cryogenic wind tunnels” Metadata:
- Title: ➤ Hot-jet simulation in cryogenic wind tunnels
- Author: Keisuke Asai
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and SpaceAdministration - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ Washington D.C - Hampton, Va - Washington, D.C - [Springfield, Va - [Washington, DC]
“Hot-jet simulation in cryogenic wind tunnels” Subjects and Themes:
- Subjects: ➤ Cryogenic wind tunnels - Exhaust flow simulation - Jet flow - Reynolds number - Wind tunnel tests - Wind tunnels
Edition Identifiers:
- The Open Library ID: ➤ OL17683287M - OL19959189M - OL13931490M - OL15576426M - OL18208937M - OL19379736M - OL18078046M - OL1812959M
- Online Computer Library Center (OCLC) ID: 20034307
- Library of Congress Control Number (LCCN): 89602567
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.
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2Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
By Marc W. Kniskern
“Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” Metadata:
- Title: ➤ Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation
- Author: Marc W. Kniskern
- Language: English
- Publisher: ➤ North Carolina State University, Dept. of Mechanical and Aerospace Engineering
- Publish Date: 1990
- Publish Location: Raleigh, [N.C.]
“Analysis of a six-component, flow-through, strain-gage, force balance used for hypersonic wind tunnel models with scramjet exhaust flow simulation” Subjects and Themes:
- Subjects: ➤ Temperature effects - Exhaust flow simulation - Force distribution - Strain gage balances - Gas injection - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18263150M - OL17632963M - OL16137883M
- Online Computer Library Center (OCLC) ID: 67142056
Access and General Info:
- First Year Published: 1990
- 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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3Radiation from advanced solid rocket motor plumes
By Richard C. Farmer
“Radiation from advanced solid rocket motor plumes” Metadata:
- Title: ➤ Radiation from advanced solid rocket motor plumes
- Author: Richard C. Farmer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - SECA, Inc.
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - Huntsville, AL - [Washington, DC
“Radiation from advanced solid rocket motor plumes” Subjects and Themes:
- Subjects: ➤ Advanced solid rocket motor (STS) - Exhaust flow simulation - Flow distribution - Radiative transfer - Rocket exhaust - Solid propellant rocket engines - Thermal radiation
Edition Identifiers:
- The Open Library ID: OL15411767M - OL17788836M
- Online Computer Library Center (OCLC) ID: 32937605
Access and General Info:
- First Year Published: 1994
- 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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4Analysis of internal flow in a ventral nozzle for STOVL aircraft
By C. Frederic Smith
“Analysis of internal flow in a ventral nozzle for STOVL aircraft” Metadata:
- Title: ➤ Analysis of internal flow in a ventral nozzle for STOVL aircraft
- Author: C. Frederic Smith
- Language: English
- Number of Pages: Median: 19
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Analysis of internal flow in a ventral nozzle for STOVL aircraft” Subjects and Themes:
- Subjects: ➤ Airplanes - Short take-off and landing aircraft - Nozzles - Ramjet engines - Numerical analysis - V/STOL aircraft - Propulsion system configurations - Ducted flow - Exhaust flow simulation - Nozzle flow - Internal flow
Edition Identifiers:
- The Open Library ID: OL17630528M - OL16137719M
- Online Computer Library Center (OCLC) ID: 24981019
Access and General Info:
- First Year Published: 1990
- 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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5High-altitude plume computer code development
By Beverly J. Audeh
“High-altitude plume computer code development” Metadata:
- Title: ➤ High-altitude plume computer code development
- Author: Beverly J. Audeh
- Language: English
- Publisher: ➤ Lockheed Missiles & Space Company, Inc., Huntsville Engineering Center
- Publish Date: 1985
- Publish Location: Huntsville, AL
“High-altitude plume computer code development” Subjects and Themes:
- Subjects: Exhaust gases - High altitude environments - Computer programs - Exhaust flow simulation - Flow distribution
Edition Identifiers:
- The Open Library ID: OL18219362M - OL16117579M
Access and General Info:
- First Year Published: 1985
- 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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6Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling
By Sanford M. Dash
“Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling” Metadata:
- Title: ➤ Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling
- Author: Sanford M. Dash
- Number of Pages: Median: 34
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: Washington, D. C
“Computer codes for HSCT exhaust flowfield simulation and observations on turbulence modeling” Subjects and Themes:
- Subjects: Turbulence models - Exhaust flow simulation
Edition Identifiers:
- The Open Library ID: OL19754274M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Measurements and predictions for velocity and turbulent kinetic energy in co-flowing air/air plumes
By K. D. Kennedy
“Measurements and predictions for velocity and turbulent kinetic energy in co-flowing air/air plumes” Metadata:
- Title: ➤ Measurements and predictions for velocity and turbulent kinetic energy in co-flowing air/air plumes
- Author: K. D. Kennedy
- Number of Pages: Median: 10
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1992
- Publish Location: Washington, D. C
“Measurements and predictions for velocity and turbulent kinetic energy in co-flowing air/air plumes” Subjects and Themes:
- Subjects: Kinetic energy - Laser velocimeters - Exhaust flow simulation
Edition Identifiers:
- The Open Library ID: OL19246749M
Access and General Info:
- First Year Published: 1992
- 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
Airflow
evacuates exhaust air. Air current Air flow meter Air handling unit Anemometer Atmosphere of Earth Computational fluid dynamics Damper (flow) Fluid dynamics
Fluid dynamics
equations. Direct numerical simulation (DNS), based on the Navier–Stokes equations, makes it possible to simulate turbulent flows at moderate Reynolds numbers
Catalytic converter
A catalytic converter part is an exhaust emission control device which converts toxic gases and pollutants in exhaust gas from an internal combustion engine
List of computer simulation software
of notable computer simulation software. Advanced Simulation Library - open-source hardware accelerated multiphysics simulation software. ASCEND - open-source
Diesel particulate filter
to remove diesel particulate matter or soot from the exhaust gas of a diesel engine. Wall-flow diesel particulate filters usually remove 85% or more
Convection (heat transfer)
of conduction (heat diffusion) and advection (heat transfer by bulk fluid flow). Convection is usually the dominant form of heat transfer in liquids and
Heat recovery ventilation
and cooling demands of buildings. By recovering the residual heat in the exhaust gas, the fresh air introduced into the air conditioning system is preheated
Diving regulator
by the ambient pressure of the exhaust and the flow resistance of the delivery system (mainly the umbilical and exhaust valve) and not much influenced
Air flow bench
for testing the intake and exhaust ports of cylinder heads of internal combustion engines. It is also used to test the flow capabilities of any component
Back pressure
to regulate flow of data, ensuring that components do not become overwhelmed. A common example of backpressure is that caused by the exhaust system (consisting