Explore: Cold Flow Tests
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Books Results
Source: The Open Library
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Search results from The Open Library
1Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube
By Jeffrey D. Wilson
“Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube” Metadata:
- Title: ➤ Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube
- Author: Jeffrey D. Wilson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Simulation of cold-test parameters and RF output power for a coupled-cavity traveling-wave tube” Subjects and Themes:
- Subjects: ➤ Radio frequencies - Computerized simulation - Cavities - Cold flow tests - Traveling wave tubes - Simulation
Edition Identifiers:
- The Open Library ID: OL17124632M - OL18118669M - OL17834466M - OL15498376M
- Online Computer Library Center (OCLC) ID: 39607562
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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2Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets
By James W. Russell
“Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets” Metadata:
- Title: ➤ Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets
- Author: James W. Russell
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Development of an empirical method for predicting jet mixing noise of cold flow rectangular jets” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aerodynamic noise - Prediction analysis techniques - Acoustic frequencies - Jet mixing flow - Cold flow tests
Edition Identifiers:
- The Open Library ID: OL15564691M - OL17594107M
- Online Computer Library Center (OCLC) ID: 43837123
Access and General Info:
- First Year Published: 1999
- 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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3Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
By George C. Olsen
“Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Metadata:
- Title: ➤ Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream
- Author: George C. Olsen
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Hydrogen file cooling with incident and swept-shock interactions in a Mach 6.4 nitrogen free stream” Subjects and Themes:
- Subjects: ➤ Hypersonic flow - Cold flow tests - Free flow - Supersonic combustion ramjet engines - Film cooling - Mass flow rate - Coolants - Oblique shock waves - Thermal protection - Gas flow - Two dimensional models - Hydrogen - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15416715M
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.
Online Borrowing:
Online Marketplaces
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4Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations
By Kevin L. Mikkelsen
“Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations” Metadata:
- Title: ➤ Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations
- Author: Kevin L. Mikkelsen
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations” Subjects and Themes:
- Subjects: Wind tunnel tests - Cold flow tests - Pressure ratio static tests - Power efficiency - Nozzle flow
Edition Identifiers:
- The Open Library ID: OL16030642M
Access and General Info:
- First Year Published: 2001
- 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 Static and wind tunnel aero-performance tests of NASA AST separate flow nozzle noise reduction configurations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Kuwait Space Rocket
that flows around the nozzle and back into the injector again. The KSR team performed a cold flow testing in October 2019 to verify the engine's flow rate
Linear Aerospike SR-71 Experiment
hot-fire flight test because of liquid oxygen leaks in the test apparatus. The ground firings and the airborne cryogenic gas flow tests provided enough
Pintle injector
rocket engine. Like any other injector, its purpose is to ensure appropriate flow rate and intermixing of the propellants as they are forcibly injected under
RP-1
engines must be ground-fired some number of times before launch. Even cold-flow tests, in which the propellants are not ignited, can leave residues. On the
NERVA
full power. A subsequent full-power Kiwi B4A test on 30 November 1962, along with a series of cold flow tests, revealed that the problem was vibrations that
ISRO
and hence the engine needs very little refurbishment. The LPSC began cold flow tests of engine prototypes in 2020. ISRO's current launch vehicles lack the
Spirometry
common of the pulmonary function tests (PFTs). It measures lung function, specifically the amount (volume) and/or speed (flow) of air that can be inhaled and
Raynaud syndrome
pallor) and becomes cold and numb. These events are episodic, and when the episode subsides or the area is warmed, the blood flow returns and the skin
Pyroclastic flow
turbulence between the flow and the overlying air, admixing and heating cold atmospheric air causing expansion and convection. Flows can deposit less than
Demonstration Rocket for Agile Cislunar Operations
will be evaluated in a cold-flow test with a nonnuclear engine mock-up to assess the mechanical integrity of the core. Such tests were conducted during