Explore: Hypersonic Wind Tunnels
Discover books, insights, and more — all in one place.
Learn more about Hypersonic Wind Tunnels with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “hypersonic-wind-tunnels”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Langley 8-ft. HTT test 139 gas analyses
By Danny R. Sprinkle
“Langley 8-ft. HTT test 139 gas analyses” Metadata:
- Title: ➤ Langley 8-ft. HTT test 139 gas analyses
- Author: Danny R. Sprinkle
- Language: English
- Number of Pages: Median: 192
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Langley 8-ft. HTT test 139 gas analyses” Subjects and Themes:
- Subjects: ➤ Hypersonic wind tunnels - Mass spectroscopy - Gas analysis - Blowdown wind tunnels - Wind tunnel calibration - Wind tunnels - Gases - Analysis
Edition Identifiers:
- The Open Library ID: ➤ OL15563082M - OL17593827M - OL17137902M - OL18139210M - OL17138164M - OL20327205M
- Online Computer Library Center (OCLC) ID: 43627661
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:
Online Marketplaces
Find Langley 8-ft. HTT test 139 gas analyses at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels
By Charles G. Miller
“Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels” Metadata:
- Title: ➤ Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels
- Author: Charles G. Miller
- Language: English
- Number of Pages: Median: 90
- Publisher: ➤ U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1981
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels” Subjects and Themes:
- Subjects: Heat - Hypersonic wind tunnels - Transmission
Edition Identifiers:
- The Open Library ID: OL15261708M - OL18023721M - OL14925818M - OL17123493M - OL17977263M
Author's Alternative Names:
"Miller, Charles G. (Charles George), 1940-" and "Miller, Charles G. 1940-"Access and General Info:
- First Year Published: 1981
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Comparison of thin-film resistance heat-transfer gages with thin-skin transient calorimeter gages in conventional hypersonic wind tunnels at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation
By Lawrence D. Huebner
“Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation” Metadata:
- Title: ➤ Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation
- Author: Lawrence D. Huebner
- Language: English
- Number of Pages: Median: 46
- Publisher: ➤ National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation” Subjects and Themes:
- Subjects: Aerodynamics, Hypersonic - Hypersonic Aerodynamics - Hypersonic wind tunnels - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL15381994M - OL14697258M - OL18062876M - OL20272564M - OL17109819M
Access and General Info:
- First Year Published: 1993
- 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 Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Aeronautical facilities catalogue
By Frank E. Peñaranda
“Aeronautical facilities catalogue” Metadata:
- Title: ➤ Aeronautical facilities catalogue
- Author: Frank E. Peñaranda
- Language: English
- Publisher: ➤ Scientific and Technical Information Branch, National Aeronautics and Space Administration - For sale by the National Technical Information Service] - For sale by the National Aeronautics and Space Administration] - For sale by the Supt. of Docs., U.S. G.P.O.]
- Publish Date: 1985 - 1986
- Publish Location: ➤ Washington, DC - [Springfield, Va
“Aeronautical facilities catalogue” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aeronautics - Catalogs - Flight simulators - Hypersonic wind tunnels - Research - Supersonic wind tunnels - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17658875M - OL17832292M - OL17667072M - OL2664364M
- Library of Congress Control Number (LCCN): 85601812
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.
Online Borrowing:
Online Marketplaces
Find Aeronautical facilities catalogue at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Enhancing U.S. competitiveness
By United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation.
“Enhancing U.S. competitiveness” Metadata:
- Title: Enhancing U.S. competitiveness
- Author: ➤ United States. Congress. House. Committee on Science, Space, and Technology. Subcommittee on Technology, Environment, and Aviation.
- Language: English
- Number of Pages: Median: 149
- Publisher: ➤ For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office - U.S. G.P.O.
- Publish Date: 1994
- Publish Location: Washington
“Enhancing U.S. competitiveness” Subjects and Themes:
- Subjects: ➤ Aeronautics - Hypersonic wind tunnels - Appropriations and expenditures - Research - United States - Aeronautics and state - Hypersonic Aerodynamics - United States. National Aeronautics and Space Administration - High-speed aeronautics - Aerodynamics, Hypersonic
- Places: United States
Edition Identifiers:
- The Open Library ID: OL1193898M - OL1206298M - OL14704276M - OL14704278M
- Online Computer Library Center (OCLC) ID: 30382697 - 30524059
- Library of Congress Control Number (LCCN): 94201122 - 94185613
- All ISBNs: 9780160441608 - 0160440947 - 9780160440946 - 0160441609
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.
Online Borrowing:
Online Marketplaces
Find Enhancing U.S. competitiveness at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium
By George C. Ashby
“Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium” Metadata:
- Title: ➤ Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium
- Author: George C. Ashby
- Language: English
- Number of Pages: Median: 60
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1977
- Publish Location: ➤ Springfield, Virginia - [Washington]
“Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium” Subjects and Themes:
- Subjects: Pressure - Hypersonic wind tunnels - Measurement
Edition Identifiers:
- The Open Library ID: OL15219010M - OL17117397M - OL18012852M
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31 ̊angle of attack and Mach 20 in helium at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7A short time response stagnation temperature probe
By R. A. East
“A short time response stagnation temperature probe” Metadata:
- Title: ➤ A short time response stagnation temperature probe
- Author: R. A. East
- Language: English
- Number of Pages: Median: 10
- Publisher: ➤ University of Southampton. Department of Aeronautics and Astronautics - H.M.S.O.
- Publish Date: 1966 - 1967
- Publish Location: London - Southampton
“A short time response stagnation temperature probe” Subjects and Themes:
- Subjects: Aerothermodynamics - Hypersonic wind tunnels - Thermocouples
Edition Identifiers:
- The Open Library ID: OL21515579M - OL5579739M
- Library of Congress Control Number (LCCN): 67093562
Access and General Info:
- First Year Published: 1966
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find A short time response stagnation temperature probe at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8A summary of design techniques for axisymmetric hypersonic wind tunnels
By Ying-Nien Yu
“A summary of design techniques for axisymmetric hypersonic wind tunnels” Metadata:
- Title: ➤ A summary of design techniques for axisymmetric hypersonic wind tunnels
- Author: Ying-Nien Yu
- Language: English
- Number of Pages: Median: 88
- Publisher: ➤ North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development - Agard
- Publish Date: 1958
- Publish Location: [Paris]
“A summary of design techniques for axisymmetric hypersonic wind tunnels” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL13957317M - OL5836554M
- Online Computer Library Center (OCLC) ID: 1846143
- Library of Congress Control Number (LCCN): 61039315
Access and General Info:
- First Year Published: 1958
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find A summary of design techniques for axisymmetric hypersonic wind tunnels at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Advanced hypersonic test facilities
By Frank K. Lu
“Advanced hypersonic test facilities” Metadata:
- Title: ➤ Advanced hypersonic test facilities
- Author: Frank K. Lu
- Language: English
- Number of Pages: Median: 632
- Publisher: ➤ AIAA (American Institute of Aeronautics & Ast - AIAA - American Institute of Aeronautics and Astronautics - AIAA (American Institute of Aeronautics & Astronautics)
- Publish Date: 2002
- Publish Location: Reston, Va
“Advanced hypersonic test facilities” Subjects and Themes:
- Subjects: ➤ Ballistic ranges - Hypersonic wind tunnels - Hypersonic Aerodynamics - Rocket sleds - Wind tunnels - Computer simulation - Ground simulators - Testing - Weapons
Edition Identifiers:
- The Open Library ID: OL23215926M - OL8644102M
- Online Computer Library Center (OCLC) ID: 51253716
- Library of Congress Control Number (LCCN): 2003271796
- All ISBNs: 1563475413 - 9781563475412
Access and General Info:
- First Year Published: 2002
- 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 Advanced hypersonic test facilities at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel
By S. Venkateswaran
“Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel” Metadata:
- Title: ➤ Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel
- Author: S. Venkateswaran
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel” Subjects and Themes:
- Subjects: Computer simulation - Hypersonic wind tunnels - Aerothermodynamics
Edition Identifiers:
- The Open Library ID: OL14683103M - OL17675808M
Access and General Info:
- First Year Published: 1992
- 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 method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31ê angle of attack and Mach 20 in helium
By George C Ashby
“Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31ê angle of attack and Mach 20 in helium” Metadata:
- Title: ➤ Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31ê angle of attack and Mach 20 in helium
- Author: George C Ashby
- Language: English
- Number of Pages: Median: 60
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration
- Publish Date: 1977
- Publish Location: [Washington] - Springfield, Va
“Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31ê angle of attack and Mach 20 in helium” Subjects and Themes:
- Subjects: Pressure - Hypersonic wind tunnels - Measurement
Edition Identifiers:
- The Open Library ID: OL14927272M - OL17977704M
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Flow-field surveys on the windward side of the NASA 040A space shuttle orbiter at 31ê angle of attack and Mach 20 in helium at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel
By Jale F. Akyurtlu
“Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel” Metadata:
- Title: ➤ Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel
- Author: Jale F. Akyurtlu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - Hampton University, Dept. of Engineering
- Publish Date: 1991 - 1993
- Publish Location: ➤ [Springfield, Va - [Hampton, Va.] - [Washington, D.C
“Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL14699054M - OL14701944M
Access and General Info:
- First Year Published: 1991
- 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 Evaluation of candidate working fluid formulations for the electrothermal-chemical wind tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Ultrasound instrumentation for the 7" Mach Seven Tunnel
By David S. Mazel
“Ultrasound instrumentation for the 7" Mach Seven Tunnel” Metadata:
- Title: ➤ Ultrasound instrumentation for the 7" Mach Seven Tunnel
- Author: David S. Mazel
- Language: English
- Publisher: ➤ Dept. of Electrical Engineering, School of Engineering, Old Dominion University
- Publish Date: 1985
- Publish Location: Norfolk, Va
“Ultrasound instrumentation for the 7" Mach Seven Tunnel” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL17832384M - OL15322568M
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.
Online Borrowing:
Online Marketplaces
Find Ultrasound instrumentation for the 7" Mach Seven Tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Nonintrusive fast response oxygen monitoring system for high temperature flows
By Daniel B. Oh
“Nonintrusive fast response oxygen monitoring system for high temperature flows” Metadata:
- Title: ➤ Nonintrusive fast response oxygen monitoring system for high temperature flows
- Author: Daniel B. Oh
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Nonintrusive fast response oxygen monitoring system for high temperature flows” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Modulation spectroscopy
Edition Identifiers:
- The Open Library ID: OL17680331M - OL14700581M
Access and General Info:
- First Year Published: 1993
- 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 Nonintrusive fast response oxygen monitoring system for high temperature flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Description and calibration of the Langley hypersonic CF
By Raymond E. Midden
“Description and calibration of the Langley hypersonic CF” Metadata:
- Title: ➤ Description and calibration of the Langley hypersonic CF
- Author: Raymond E. Midden
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Description and calibration of the Langley hypersonic CF” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL14662946M - OL15274112M
Access and General Info:
- First Year Published: 1987
- 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 Description and calibration of the Langley hypersonic CF at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42)
By J. Marroquin
“Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42)” Metadata:
- Title: ➤ Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42)
- Author: J. Marroquin
- Language: English
- Publisher: ➤ Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration
- Publish Date: 1985
- Publish Location: Houston, Tex
“Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42)” Subjects and Themes:
- Subjects: Transmission - Hypersonic wind tunnels - Heat
Edition Identifiers:
- The Open Library ID: OL18221273M - OL16119769M
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.
Online Borrowing:
Online Marketplaces
Find Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms
By Nathan S. Jacobson
“Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms” Metadata:
- Title: ➤ Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms
- Author: Nathan S. Jacobson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Cleveland, Ohio] - [Springfield, Va
“Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Graphite - Furnaces
Edition Identifiers:
- The Open Library ID: OL17839427M - OL15548960M
- Online Computer Library Center (OCLC) ID: 42045747
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:
Online Marketplaces
Find Plumbrook Hypersonic Tunnel Facility graphite furnace degradation mechanisms at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flows
By Robert L. McKenzie
“Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flows” Metadata:
- Title: ➤ Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flows
- Author: Robert L. McKenzie
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flows” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Laser spectroscopy
Edition Identifiers:
- The Open Library ID: OL18052351M - OL15357255M
Access and General Info:
- First Year Published: 1992
- 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 Laser-spectroscopic measurement techniques for hypersonic, turbulent wind tunnel flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
By Scott Douglas Holland
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:
- Title: ➤ Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
- Author: Scott Douglas Holland
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Subjects and Themes:
- Subjects: ➤ Inlet flow - Actuators - Hypersonic wind tunnels - Supersonic combustion ramjet engines - Blocking - Engine inlets - Hypersonic inlets - Cowlings - Wind tunnel tests - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL15409524M - OL18079126M
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.
Online Borrowing:
Online Marketplaces
Find Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
20Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly
By Gregory J. Brauckmann
“Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly” Metadata:
- Title: ➤ Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly
- Author: Gregory J. Brauckmann
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - American Institute of Aeronautics and Astronautics - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Washington, DC - Springfield, Va
“Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly” Subjects and Themes:
- Subjects: ➤ Space shuttle orbiters - Temperature effects - Pitching moments - Wind tunnel tests - Flow distribution - Ideal gas - Gas flow - Navier-Stokes equation - Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL15498438M - OL17837132M
- Online Computer Library Center (OCLC) ID: 39777210
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
Find Experimental and computational analysis of shuttle orbiter hypersonic trim anomaly at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21Development of the spark-heated, hypervelocity, blowdown tunnel-Hotshot
By R. W. Perry
“Development of the spark-heated, hypervelocity, blowdown tunnel-Hotshot” Metadata:
- Title: ➤ Development of the spark-heated, hypervelocity, blowdown tunnel-Hotshot
- Author: R. W. Perry
- Language: English
- Number of Pages: Median: 103
- Publisher: AF-AEDC
- Publish Date: 1958
- Publish Location: Tullahoma, Tenn
“Development of the spark-heated, hypervelocity, blowdown tunnel-Hotshot” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL21694072M
Access and General Info:
- First Year Published: 1958
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Development of the spark-heated, hypervelocity, blowdown tunnel-Hotshot at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
22On the equilibrium piston technique in gun tunnels
By L. Davies
“On the equilibrium piston technique in gun tunnels” Metadata:
- Title: ➤ On the equilibrium piston technique in gun tunnels
- Author: L. Davies
- Language: English
- Number of Pages: Median: 18
- Publisher: H.M.S.O.
- Publish Date: 1968
- Publish Location: London
“On the equilibrium piston technique in gun tunnels” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Shock tubes
Edition Identifiers:
- The Open Library ID: OL5770076M
- Library of Congress Control Number (LCCN): 71475412
Access and General Info:
- First Year Published: 1968
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find On the equilibrium piston technique in gun tunnels at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23Determination of stagnation temperatures in the R.A.R.D.E. hypersonic gun tunnel from streak camera measurements of flow velocity
By Bowman, J. E.
“Determination of stagnation temperatures in the R.A.R.D.E. hypersonic gun tunnel from streak camera measurements of flow velocity” Metadata:
- Title: ➤ Determination of stagnation temperatures in the R.A.R.D.E. hypersonic gun tunnel from streak camera measurements of flow velocity
- Author: Bowman, J. E.
- Language: English
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“Determination of stagnation temperatures in the R.A.R.D.E. hypersonic gun tunnel from streak camera measurements of flow velocity” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL4617158M
- Library of Congress Control Number (LCCN): 77403735
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Determination of stagnation temperatures in the R.A.R.D.E. hypersonic gun tunnel from streak camera measurements of flow velocity at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
24Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel
By Bowman, J. E.
“Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel” Metadata:
- Title: ➤ Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel
- Author: Bowman, J. E.
- Language: English
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel” Subjects and Themes:
- Subjects: Condensation - Hypersonic wind tunnels - Nitrogen
Edition Identifiers:
- The Open Library ID: OL5674387M
- Library of Congress Control Number (LCCN): 68136850
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
25Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle
By Harris M. Schurmeier
“Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle” Metadata:
- Title: ➤ Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle
- Author: Harris M. Schurmeier
- Language: English
- Number of Pages: Median: 156
- Publisher: ➤ North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development
- Publish Date: 1959
- Publish Location: [Paris]
“Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL5793123M
- Online Computer Library Center (OCLC) ID: 1844489
- Library of Congress Control Number (LCCN): 60004358
Access and General Info:
- First Year Published: 1959
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Design and operation of a continuous-flow hypersonic wind tunnel using a two-dimensional nozzle at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
26A study on the running times in reflected shock tunnels
By J. A. D. Ackroyd
“A study on the running times in reflected shock tunnels” Metadata:
- Title: ➤ A study on the running times in reflected shock tunnels
- Author: J. A. D. Ackroyd
- Language: English
- Number of Pages: Median: 17
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“A study on the running times in reflected shock tunnels” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Shock tubes
Edition Identifiers:
- The Open Library ID: OL5579694M
- Library of Congress Control Number (LCCN): 67093511
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find A study on the running times in reflected shock tunnels at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
27Bulk compressibility effects in the R.A.R.D.E. no. 3 hypersonic gun tunnel
By W. A. Clayden
“Bulk compressibility effects in the R.A.R.D.E. no. 3 hypersonic gun tunnel” Metadata:
- Title: ➤ Bulk compressibility effects in the R.A.R.D.E. no. 3 hypersonic gun tunnel
- Author: W. A. Clayden
- Language: English
- Number of Pages: Median: 13
- Publisher: H.M.S.O.
- Publish Date: 1966
- Publish Location: London
“Bulk compressibility effects in the R.A.R.D.E. no. 3 hypersonic gun tunnel” Subjects and Themes:
- Subjects: Compressibility - Gas dynamics - Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL5579820M
- Library of Congress Control Number (LCCN): 67093692
Access and General Info:
- First Year Published: 1966
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Bulk compressibility effects in the R.A.R.D.E. no. 3 hypersonic gun tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
28Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4
By Henry T. Nagamatsu
“Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4” Metadata:
- Title: ➤ Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4
- Author: Henry T. Nagamatsu
- Language: English
- Number of Pages: Median: 45
- Publisher: ➤ National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.]
- Publish Date: 1970
- Publish Location: Washington
“Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4” Subjects and Themes:
- Subjects: Heat - Hypersonic wind tunnels - Rarefied gas dynamics - Transmission
Edition Identifiers:
- The Open Library ID: OL5276059M
- Library of Congress Control Number (LCCN): 71610044
Access and General Info:
- First Year Published: 1970
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Heat transfer on a flat plate in continuum to rarefied hypersonic flows at Mach numbers of 19.2 and 25.4 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
29Advanced experimental techniques for study of hypervelocity flight
By Hypervelocity Techniques Symposium (4th 1965 Arnold Engineering Development Center)
“Advanced experimental techniques for study of hypervelocity flight” Metadata:
- Title: ➤ Advanced experimental techniques for study of hypervelocity flight
- Author: ➤ Hypervelocity Techniques Symposium (4th 1965 Arnold Engineering Development Center)
- Language: English
- Number of Pages: Median: 631
- Publisher: Denver Research Institute
- Publish Date: 1965
- Publish Location: Denver
“Advanced experimental techniques for study of hypervelocity flight” Subjects and Themes:
- Subjects: Hypersonic Aerodynamics - Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL5529763M
- Online Computer Library Center (OCLC) ID: 2899143
- Library of Congress Control Number (LCCN): 67004624
Access and General Info:
- First Year Published: 1965
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Advanced experimental techniques for study of hypervelocity flight at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
30Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF?□Tunnel
By R. A. Thompson
“Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF?□Tunnel” Metadata:
- Title: ➤ Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF?□Tunnel
- Author: R. A. Thompson
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF?□Tunnel” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL17095074M
Access and General Info:
- First Year Published: 1987
- 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 analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF?□Tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
31Factors in the design of a hypersonic tunnel
By G. V. Bull
“Factors in the design of a hypersonic tunnel” Metadata:
- Title: ➤ Factors in the design of a hypersonic tunnel
- Author: G. V. Bull
- Number of Pages: Median: 55
- Publisher: Sine nomine
- Publish Date: 1949
- Publish Location: [Downsview, Ont.]
“Factors in the design of a hypersonic tunnel” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL20985058M
Access and General Info:
- First Year Published: 1949
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Factors in the design of a hypersonic tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
32Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF
By R. A. Thompson
“Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF” Metadata:
- Title: ➤ Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF
- Author: R. A. Thompson
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Computational analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL14661663M
Access and General Info:
- First Year Published: 1987
- 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 analysis and preliminary redesign of the nozzle contour of the Langley Hypersonic CF at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33Into the wind
By J. Lawrence Lee
“Into the wind” Metadata:
- Title: Into the wind
- Author: J. Lawrence Lee
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Communications, History Program Office
- Publish Date: 2012
- Publish Location: Washington, DC
“Into the wind” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL25025280M
- Library of Congress Control Number (LCCN): 2011032839
Access and General Info:
- First Year Published: 2012
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Into the wind at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
34PSL
By Robert S. Arrighi
“PSL” Metadata:
- Title: PSL
- Author: Robert S. Arrighi
- Language: English
- Number of Pages: Median: 185
- Publisher: ➤ National Aeronautics and Space Administration, NASA History Division, Office of External Relations
- Publish Date: 2012
- Publish Location: Washington, DC
“PSL” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Hypersonic wind tunnels - Wind tunnels - Research - Propulsion Systems Laboratory (U.S.) - NASA Glenn Research Center - History - Propulsion systems
- Places: United States
- Time: 20th century
Edition Identifiers:
- The Open Library ID: OL25018510M
- Online Computer Library Center (OCLC) ID: 748941698
- Library of Congress Control Number (LCCN): 2011032380
Access and General Info:
- First Year Published: 2012
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find PSL at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
35Survey of short duration, hypersonic and hypervelocity facilities
By Frank K. Lu
“Survey of short duration, hypersonic and hypervelocity facilities” Metadata:
- Title: ➤ Survey of short duration, hypersonic and hypervelocity facilities
- Author: Frank K. Lu
- Number of Pages: Median: 12
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1994
- Publish Location: Washington, D. C
“Survey of short duration, hypersonic and hypervelocity facilities” Subjects and Themes:
- Subjects: Hypervelocity wind tunnels - Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL19001391M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Survey of short duration, hypersonic and hypervelocity facilities at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
36Real gas flow parameters for NASA Langley 22-inch Mach 20 helium tunnel
By Brian R. Hollis
“Real gas flow parameters for NASA Langley 22-inch Mach 20 helium tunnel” Metadata:
- Title: ➤ Real gas flow parameters for NASA Langley 22-inch Mach 20 helium tunnel
- Author: Brian R. Hollis
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Real gas flow parameters for NASA Langley 22-inch Mach 20 helium tunnel” Subjects and Themes:
- Subjects: Gases, Real - Hypersonic wind tunnels - Real Gases
Edition Identifiers:
- The Open Library ID: OL15366981M
Access and General Info:
- First Year Published: 1992
- 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 Real gas flow parameters for NASA Langley 22-inch Mach 20 helium tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
37Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels
By Gregory M. Buck
“Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels” Metadata:
- Title: ➤ Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels
- Author: Gregory M. Buck
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels” Subjects and Themes:
- Subjects: Surface temperature - Pressure measurement - Hypersonic wind tunnels - Photoluminescence - Temperature measurement
Edition Identifiers:
- The Open Library ID: OL15501806M
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
Find Simultaneous luminescence pressure and temperature measurement system for hypersonic wind tunnels at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
38Modification of NASA Langley 8-foot high temperature tunnel to provide a unique national research facility for hypersonic air-breathing propulsion systems
By H. Neale Kelly
“Modification of NASA Langley 8-foot high temperature tunnel to provide a unique national research facility for hypersonic air-breathing propulsion systems” Metadata:
- Title: ➤ Modification of NASA Langley 8-foot high temperature tunnel to provide a unique national research facility for hypersonic air-breathing propulsion systems
- Author: H. Neale Kelly
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1984
- Publish Location: Hampton, Va
“Modification of NASA Langley 8-foot high temperature tunnel to provide a unique national research facility for hypersonic air-breathing propulsion systems” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Space vehicles - Propulsion systems
Edition Identifiers:
- The Open Library ID: OL14926345M
Access and General Info:
- First Year Published: 1984
- 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 Modification of NASA Langley 8-foot high temperature tunnel to provide a unique national research facility for hypersonic air-breathing propulsion systems at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
39Third Hypervelocity Techniques Symposium
By Hypervelocity Techniques Symposium. (3d 1964 Denver, Colo.)
“Third Hypervelocity Techniques Symposium” Metadata:
- Title: ➤ Third Hypervelocity Techniques Symposium
- Author: ➤ Hypervelocity Techniques Symposium. (3d 1964 Denver, Colo.)
- Language: English
- Publisher: Denver Research Institute
- Publish Date: 1964
- Publish Location: Denver
“Third Hypervelocity Techniques Symposium” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL18824138M
Access and General Info:
- First Year Published: 1964
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Third Hypervelocity Techniques Symposium at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
40Fourth Hypervelocity Techniques Symposium
By Hypervelocity Techniques Symposium. (4th 1965 Arnold Engineering Development Center)
“Fourth Hypervelocity Techniques Symposium” Metadata:
- Title: ➤ Fourth Hypervelocity Techniques Symposium
- Author: ➤ Hypervelocity Techniques Symposium. (4th 1965 Arnold Engineering Development Center)
- Language: English
- Number of Pages: Median: 631
- Publisher: Denver Research Institute
- Publish Date: 1965
- Publish Location: Denver
“Fourth Hypervelocity Techniques Symposium” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL18824153M
Access and General Info:
- First Year Published: 1965
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Fourth Hypervelocity Techniques Symposium at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
41Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
By Scott D. Holland
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Metadata:
- Title: ➤ Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
- Author: Scott D. Holland
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6” Subjects and Themes:
- Subjects: ➤ Inlet flow - Actuators - Hypersonic wind tunnels - Supersonic combustion ramjet engines - Blocking - Engine inlets - Hypersonic inlets - Cowlings - Wind tunnel tests - Shock wave interaction
Edition Identifiers:
- The Open Library ID: OL17114738M
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.
Online Borrowing:
Online Marketplaces
Find Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
42Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center
By C. G. Miller
“Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center” Metadata:
- Title: ➤ Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center
- Author: C. G. Miller
- Number of Pages: Median: 30
- Publisher: AIAA
- Publish Date: 1992
- Publish Location: Washington
“Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Langley Research Center
Edition Identifiers:
- The Open Library ID: OL19247529M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Hypersonic aerodynamic/aerothermodynamic testing capabilities at Langley Research Center at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
43Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facility
By Jose Tamagno
“Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facility” Metadata:
- Title: ➤ Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facility
- Author: Jose Tamagno
- Number of Pages: Median: 10
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1990
- Publish Location: Washington, D. C
“Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facility” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Hypersonic combustion - Hypervelocity flow
Edition Identifiers:
- The Open Library ID: OL19246743M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Hypervelocity real gas capabilities of GASL's expansion tube (HYPULSE) facility at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
44Mach 5 electroformed nickel nozzle refurbishment
By Robert Rood
“Mach 5 electroformed nickel nozzle refurbishment” Metadata:
- Title: ➤ Mach 5 electroformed nickel nozzle refurbishment
- Author: Robert Rood
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1992
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Mach 5 electroformed nickel nozzle refurbishment” Subjects and Themes:
- Subjects: Hypersonic wind tunnels - Metal coating
Edition Identifiers:
- The Open Library ID: OL14688957M
Access and General Info:
- First Year Published: 1992
- 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 Mach 5 electroformed nickel nozzle refurbishment at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
45Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C)
By J. Marroquin
“Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C)” Metadata:
- Title: ➤ Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C)
- Author: J. Marroquin
- Language: English
- Publisher: ➤ Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration
- Publish Date: 1985
- Publish Location: Houston, Tex
“Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C)” Subjects and Themes:
- Subjects: ➤ Hypersonic wind tunnels - Supersonic wind tunnels - Von Karman Institute for Fluid Dynamics
Edition Identifiers:
- The Open Library ID: OL16119765M
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.
Online Borrowing:
Online Marketplaces
Find Results of aeroheating DFI and ET design-data test on a 0.0175-scale model 60-OTS conducted in the Von Karman gas dynamics facility (VKF) 40-inch supersonic and the 50-inch hypersonic wind tunnels A&C (IH-97A/B/C) at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
46Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing
By David E. Reubush
“Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing” Metadata:
- Title: ➤ Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing
- Author: David E. Reubush
- Language: English
- Number of Pages: Median: 11
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va - [Springfield, Va
“Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing” Subjects and Themes:
- Subjects: Aerodynamics, Hypersonic - Ground tests - Hypersonic Aerodynamics - Hypersonic wind tunnels - Propulsion system configurations
Edition Identifiers:
- The Open Library ID: OL17115184M
Access and General Info:
- First Year Published: 1987
- 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 Modification to the Langley 8-foot high temperature tunnel for hypersonic propulsion testing at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
47The development of a hypersonic wind tunnel
By D. H. Henshaw
“The development of a hypersonic wind tunnel” Metadata:
- Title: ➤ The development of a hypersonic wind tunnel
- Author: D. H. Henshaw
- Publisher: [Institute of Aerophysics]
- Publish Date: 1950
- Publish Location: [Downsview, Ont.]
“The development of a hypersonic wind tunnel” Subjects and Themes:
- Subjects: Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL19986965M
Access and General Info:
- First Year Published: 1950
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find The development of a hypersonic wind tunnel at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
48Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21)
By A. M. Springer
“Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21)” Metadata:
- Title: ➤ Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21)
- Author: A. M. Springer
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 1998
- Publish Location: ➤ Springfield, VA - [Huntsville, Ala.]
“Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21)” Subjects and Themes:
- Subjects: ➤ Photopolymers - Supersonic wind tunnels - Laminates - Nylon (Trademark) - Hypersonic wind tunnels - Wind tunnel tests - Body-wing and tail configurations
Edition Identifiers:
- The Open Library ID: OL15542765M
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:
Online Marketplaces
Find Application of rapid prototyping methods to high-speed wind tunnel testing (MSFC Center Director's Discretionary Fund final report, project no. 96-21) at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
49Arc heaters and MHD accelerators for aerodynamic purposes
By Arnold Engineering Development Center.
“Arc heaters and MHD accelerators for aerodynamic purposes” Metadata:
- Title: ➤ Arc heaters and MHD accelerators for aerodynamic purposes
- Author: ➤ Arnold Engineering Development Center.
- Language: English
- Number of Pages: Median: 174
- Publisher: ➤ North Atlantic Treaty Organization, Advisory Group for Aeronautical Research and Development]
- Publish Date: 1964
- Publish Location: [Paris
“Arc heaters and MHD accelerators for aerodynamic purposes” Subjects and Themes:
- Subjects: Plasma accelerators - Hypersonic wind tunnels
Edition Identifiers:
- The Open Library ID: OL20666679M
Access and General Info:
- First Year Published: 1964
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Arc heaters and MHD accelerators for aerodynamic purposes at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
50Advanced experimental techniques for study of hypervelocity flight
By Hypervelocity Techniques Symposium. (5th 1967 University of Denver)
“Advanced experimental techniques for study of hypervelocity flight” Metadata:
- Title: ➤ Advanced experimental techniques for study of hypervelocity flight
- Author: ➤ Hypervelocity Techniques Symposium. (5th 1967 University of Denver)
- Language: English
- Publisher: Denver Research Institute
- Publish Date: 1967
- Publish Location: Denver
“Advanced experimental techniques for study of hypervelocity flight” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL20797528M
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Advanced experimental techniques for study of hypervelocity flight at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.