Explore: Supersonic Aircraft
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Source: The Open Library
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1Lateral-directional eigenvector flying qualities guidelines for high performance aircraft
By John B. Davidson
“Lateral-directional eigenvector flying qualities guidelines for high performance aircraft” Metadata:
- Title: ➤ Lateral-directional eigenvector flying qualities guidelines for high performance aircraft
- Author: John B. Davidson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Lateral-directional eigenvector flying qualities guidelines for high performance aircraft” Subjects and Themes:
- Subjects: Eigenvectors - Supersonic aircraft - Flight characteristics - Fighter aircraft - Lateral stability
Edition Identifiers:
- The Open Library ID: OL18118595M - OL17125029M - OL15498128M - OL17565039M
- Online Computer Library Center (OCLC) ID: 39693592
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
By Charles J. Trefny
“Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets” Metadata:
- Title: ➤ Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
- Author: Charles J. Trefny
- Language: English
- Number of Pages: Median: 60
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Lewis Research Center
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - Springfield, Va - Cleveland, Ohio
“Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets” Subjects and Themes:
- Subjects: ➤ Supersonic inlets - Supersonic aircraft - Internal compression inlets - Air intakes - Aerodynamics - Low speed - Jet engines
Edition Identifiers:
- The Open Library ID: OL18218668M - OL19985907M - OL16116660M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Full flight envelope direct thrust measurement on a supersonic aircraft
By Timothy R. Conners
“Full flight envelope direct thrust measurement on a supersonic aircraft” Metadata:
- Title: ➤ Full flight envelope direct thrust measurement on a supersonic aircraft
- Author: Timothy R. Conners
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1998
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Full flight envelope direct thrust measurement on a supersonic aircraft” Subjects and Themes:
- Subjects: F-15 aircraft - Supersonic aircraft - Mach number - Turbofan engines
Edition Identifiers:
- The Open Library ID: OL15544011M - OL17838340M
- Online Computer Library Center (OCLC) ID: 41019967
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Supersonic wing and wing-body shape optimization using an adjoint formulation
By James Reuther
“Supersonic wing and wing-body shape optimization using an adjoint formulation” Metadata:
- Title: ➤ Supersonic wing and wing-body shape optimization using an adjoint formulation
- Author: James Reuther
- Language: English
- Publisher: ➤ Research Institute for Advanced Computer Science, NASA Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Moffett Field, Calif.]
“Supersonic wing and wing-body shape optimization using an adjoint formulation” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic aircraft - Body-wing configurations - Supersonic flow - Three dimensional flow - Control theory - Optimization - Euler equations of motion - Aerodynamic configurations - Aircraft design - Wings - Supersonic airfoils
Edition Identifiers:
- The Open Library ID: OL18084750M - OL15419682M - OL17076145M
- Online Computer Library Center (OCLC) ID: 34762339
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Changing the landscape of civil aviation
By Carol J. Russo
“Changing the landscape of civil aviation” Metadata:
- Title: ➤ Changing the landscape of civil aviation
- Author: Carol J. Russo
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Changing the landscape of civil aviation” Subjects and Themes:
- Subjects: Supersonic aircraft - Propulsion - Air breathing engines - Civil aviation - General aviation aircraft
Edition Identifiers:
- The Open Library ID: OL15539867M
- Online Computer Library Center (OCLC) ID: 40758966
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Development of techniques for the in situ observation of OH and HO₂ for studies of the impact of high-altitude supersonic aircraft on the stratosphere
final technical report
By James G. Anderson
“Development of techniques for the in situ observation of OH and HO₂ for studies of the impact of high-altitude supersonic aircraft on the stratosphere” Metadata:
- Title: ➤ Development of techniques for the in situ observation of OH and HO₂ for studies of the impact of high-altitude supersonic aircraft on the stratosphere
- Author: James G. Anderson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Development of techniques for the in situ observation of OH and HO₂ for studies of the impact of high-altitude supersonic aircraft on the stratosphere” Subjects and Themes:
- Subjects: ➤ Supersonic aircraft - Atmospheric chemistry - Laser induced fluorescence - High altitude - Spacecraft instruments - Water - Photochemical reactions - Air sampling - Hydroxyl emission - Effluents
Edition Identifiers:
- The Open Library ID: OL17001388M - OL17682887M
- Online Computer Library Center (OCLC) ID: 32214429
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Evaluation of frameworks for HSCT design optimization
By Ramki Krishnan
“Evaluation of frameworks for HSCT design optimization” Metadata:
- Title: ➤ Evaluation of frameworks for HSCT design optimization
- Author: Ramki Krishnan
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - [Springfield, Va
“Evaluation of frameworks for HSCT design optimization” Subjects and Themes:
- Subjects: Supersonic aircraft - Aircraft design - Computer aided design - Multidisciplinary design optimization
Edition Identifiers:
- The Open Library ID: OL17839120M - OL15544695M
- Online Computer Library Center (OCLC) ID: 41347635
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Supersonic jet exhaust noise investigation
By P. R. Knott
“Supersonic jet exhaust noise investigation” Metadata:
- Title: ➤ Supersonic jet exhaust noise investigation
- Author: P. R. Knott
- Number of Pages: Median: 268
- Publisher: ➤ General Electric Company, Aircraft Engine Group, Advanced Engineering and Technical Programs Dept - Air Force Aero Propulsion Laboratory, Air Force Systems Command
- Publish Date: 1974 - 1976
- Publish Location: ➤ Wright-Patterson AFB, Ohio - Cincinnati, Ohio
“Supersonic jet exhaust noise investigation” Subjects and Themes:
- Subjects: Jet aircraft noise - Supersonic aircraft - Jet exhaust - Supersonic jet flow
Edition Identifiers:
- The Open Library ID: OL19045205M - OL20268622M
Access and General Info:
- First Year Published: 1974
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Proceedings
By Conference on Sonic Boom Research Washington, D.C. 1968.
“Proceedings” Metadata:
- Title: Proceedings
- Author: ➤ Conference on Sonic Boom Research Washington, D.C. 1968.
- Language: English
- Number of Pages: Median: 193
- Publisher: ➤ Scientific and Technical Information Division, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.]
- Publish Date: 1968
- Publish Location: Washington
“Proceedings” Subjects and Themes:
- Subjects: Congresses - Sonic boom - Noise - Supersonic aircraft - Conferences
Edition Identifiers:
- The Open Library ID: OL5634991M
- Online Computer Library Center (OCLC) ID: 70935926
- Library of Congress Control Number (LCCN): 68062087
Access and General Info:
- First Year Published: 1968
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data
By Vladislav Klein
“Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data” Metadata:
- Title: ➤ Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data
- Author: Vladislav Klein
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Aerodynamic parameters of high performance aircraft estimated from wind tunnel and flight test data” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Fighter aircraft - Supersonic aircraft - Unsteady aerodynamics - X-29 aircraft - X-31 aircraft
Edition Identifiers:
- The Open Library ID: OL15542100M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Concept development of a Mach 2.4 high-speed civil transport
“Concept development of a Mach 2.4 high-speed civil transport” Metadata:
- Title: ➤ Concept development of a Mach 2.4 high-speed civil transport
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: [Springfield, Va - Hampton, Va
“Concept development of a Mach 2.4 high-speed civil transport” Subjects and Themes:
- Subjects: ➤ Supersonic speed - High speed - Supersonic cruise aircraft research - Supersonic transports - Supersonic aircraft - Transport aircraft - Aircraft design
Edition Identifiers:
- The Open Library ID: OL15569353M
- Online Computer Library Center (OCLC) ID: 44447753
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Assessment of NASA's aircraft noise prediction capability
By Milo D. Dahl
“Assessment of NASA's aircraft noise prediction capability” Metadata:
- Title: ➤ Assessment of NASA's aircraft noise prediction capability
- Author: Milo D. Dahl
- Language: English
- Number of Pages: Median: 354
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2012
- Publish Location: Cleveland, Ohio
“Assessment of NASA's aircraft noise prediction capability” Subjects and Themes:
- Subjects: ➤ Jet planes - Noise - Aeroacoustics - Noise prediction (aircraft) - Jet aircraft noise - Wind tunnel tests - Hypersonic aircraft - Subsonic aircraft - Rotary wing aircraft - Computational fluid dynamics - Aircraft noise - Supersonic aircraft
Edition Identifiers:
- The Open Library ID: OL31033961M
- Online Computer Library Center (OCLC) ID: 818645984 - 823318882
- Library of Congress Control Number (LCCN): 2012515605
Access and General Info:
- First Year Published: 2012
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13A preliminary evaluation of 1. Noise, 2. Air pollution, 3. Stratospheric effects, related to SST operations
By W. D. Miller
“A preliminary evaluation of 1. Noise, 2. Air pollution, 3. Stratospheric effects, related to SST operations” Metadata:
- Title: ➤ A preliminary evaluation of 1. Noise, 2. Air pollution, 3. Stratospheric effects, related to SST operations
- Author: W. D. Miller
- Number of Pages: Median: 17
- Publisher: ➤ Aviation Planning and Research Division, Civil Aviation Branch, Canadian Air Transportation Administration
- Publish Date: 1971
- Publish Location: [Ottawa]
“A preliminary evaluation of 1. Noise, 2. Air pollution, 3. Stratospheric effects, related to SST operations” Subjects and Themes:
- Subjects: Supersonic aircraft - Aircraft noise - Stratosphere - Supersonic transports - Air pollution
Edition Identifiers:
- The Open Library ID: OL22344729M
Access and General Info:
- First Year Published: 1971
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14The atmospheric effects of stratospheric aircraft: a current consensus
By A. R. Douglass
“The atmospheric effects of stratospheric aircraft: a current consensus” Metadata:
- Title: ➤ The atmospheric effects of stratospheric aircraft: a current consensus
- Author: A. R. Douglass
- Number of Pages: Median: 39
- Publisher: ➤ NASA, Office of Space Science and Applications
- Publish Date: 1991
- Publish Location: Washington, D. C
“The atmospheric effects of stratospheric aircraft: a current consensus” Subjects and Themes:
- Subjects: Atmospheric effects - Stratosphere - Supersonic aircraft - Upper Atmosphere
Edition Identifiers:
- The Open Library ID: OL21335034M
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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15The generation and radiation of supersonic jet noise
By Air Force Aero Propulsion Laboratory (U.S.)
“The generation and radiation of supersonic jet noise” Metadata:
- Title: ➤ The generation and radiation of supersonic jet noise
- Author: ➤ Air Force Aero Propulsion Laboratory (U.S.)
- Publisher: ➤ Air Force Aero-Propulsion Laboratories
- Publish Date: 1976
- Publish Location: ➤ Wright-Patterson Air Force Base, Ohio
“The generation and radiation of supersonic jet noise” Subjects and Themes:
- Subjects: Supersonic aircraft - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL19045148M
Access and General Info:
- First Year Published: 1976
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16The generation and radiation of supersonic jet noise
By Harry E. Plumblee
“The generation and radiation of supersonic jet noise” Metadata:
- Title: ➤ The generation and radiation of supersonic jet noise
- Author: Harry E. Plumblee
- Publisher: ➤ Air Force Aero Propulsion Laboratory
- Publish Date: 1972
- Publish Location: ➤ Wright-Patterson Air Force Base, Ohio
“The generation and radiation of supersonic jet noise” Subjects and Themes:
- Subjects: Supersonic aircraft - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL19045165M
Access and General Info:
- First Year Published: 1972
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17The atmospheric effects of stratospheric aircraft: a first program report
By Michael J. Prather
“The atmospheric effects of stratospheric aircraft: a first program report” Metadata:
- Title: ➤ The atmospheric effects of stratospheric aircraft: a first program report
- Author: Michael J. Prather
- Number of Pages: Median: 233
- Publisher: ➤ NASA, Office of Space Science and Applications
- Publish Date: 1992
- Publish Location: Washington, D. C
“The atmospheric effects of stratospheric aircraft: a first program report” Subjects and Themes:
- Subjects: Aerosols - Atmospheric effects - Supersonic aircraft - Upper Atmosphere
Edition Identifiers:
- The Open Library ID: OL21378572M
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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18Parallelization of a parabolized Navier-Stokes solver with a design optimizer
By J. M. Pallis
“Parallelization of a parabolized Navier-Stokes solver with a design optimizer” Metadata:
- Title: ➤ Parallelization of a parabolized Navier-Stokes solver with a design optimizer
- Author: J. M. Pallis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Parallelization of a parabolized Navier-Stokes solver with a design optimizer” Subjects and Themes:
- Subjects: ➤ Supersonic aircraft - Hypersonic flow - Aerodynamics - Supersonic flow - Aircraft design - Supersonic transports - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15487262M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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19The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts
By Alexander M. Starik
“The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts” Metadata:
- Title: ➤ The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts
- Author: Alexander M. Starik
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts” Subjects and Themes:
- Subjects: ➤ Supersonic aircraft - Internal flow - Plumes - Hypersonics - Kinetics - Nonequilibrium conditions
Edition Identifiers:
- The Open Library ID: OL15543552M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Advances in experiment design for high performance aircraft
By Engene A. Morelli
“Advances in experiment design for high performance aircraft” Metadata:
- Title: ➤ Advances in experiment design for high performance aircraft
- Author: Engene A. Morelli
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Advances in experiment design for high performance aircraft” Subjects and Themes:
- Subjects: Supersonic aircraft - F-18 aircraft - Cramer-Rao bounds - Research vehicles
Edition Identifiers:
- The Open Library ID: OL15541879M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47
By Francis J. Capone
“Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47” Metadata:
- Title: ➤ Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47
- Author: Francis J. Capone
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Aerodynamic characteristics of a supersonic fighter aircraft model at Mach 0.40 to 2.47” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamics, Supersonic - Data bases - Databases - Fighter aircraft - Supersonic Aerodynamics - Supersonic aircraft - Supersonic fighter planes
Edition Identifiers:
- The Open Library ID: OL18218665M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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22NASA-UVa Light Aerospace Alloy and Structure Technology Program supplement: aluminum-based materials for high speed aircraft
By E. A. Starke
“NASA-UVa Light Aerospace Alloy and Structure Technology Program supplement: aluminum-based materials for high speed aircraft” Metadata:
- Title: ➤ NASA-UVa Light Aerospace Alloy and Structure Technology Program supplement: aluminum-based materials for high speed aircraft
- Author: E. A. Starke
- Number of Pages: Median: 221
- Publisher: Langley Research Center
- Publish Date: 1993
- Publish Location: Hampton, Va
“NASA-UVa Light Aerospace Alloy and Structure Technology Program supplement: aluminum-based materials for high speed aircraft” Subjects and Themes:
- Subjects: Supersonic aircraft - Aluminum alloys
Edition Identifiers:
- The Open Library ID: OL19916481M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration
By Mike C. Fox
“Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration” Metadata:
- Title: ➤ Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration
- Author: Mike C. Fox
- Number of Pages: Median: 117
- Publisher: Langley Research Center
- Publish Date: 1993
- Publish Location: Hampton, Va
“Supersonic aerodynamic characteristics of an advanced F-16 derivative aircraft configuration” Subjects and Themes:
- Subjects: Supersonic aircraft - F-16 aircraft - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL19916539M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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24Flight test measurements from the Tu-144LL structure/cabin noise experiment
By Stephen A. Rizzi
“Flight test measurements from the Tu-144LL structure/cabin noise experiment” Metadata:
- Title: ➤ Flight test measurements from the Tu-144LL structure/cabin noise experiment
- Author: Stephen A. Rizzi
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2000
- Publish Location: [Springfield, Va - Hampton, Va
“Flight test measurements from the Tu-144LL structure/cabin noise experiment” Subjects and Themes:
- Subjects: ➤ Acceleration measurement - Supersonic aircraft - Aircraft noise - Aircraft structures - Tupolev aircraft - Flight tests
Edition Identifiers:
- The Open Library ID: OL15574422M
Access and General Info:
- First Year Published: 2000
- 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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25Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
By Eric F. Charlton
“Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models” Metadata:
- Title: ➤ Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models
- Author: Eric F. Charlton
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - Springfield, VA
“Numerical stability and control analysis towards falling-leaf prediction capabilities of splitflow for two generic high-performance aircraft models” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Computational fluid dynamics - Supersonic aircraft - Aircraft models - Design analysis - Angle of attack - Aerodynamic characteristics - Fighter aircraft
Edition Identifiers:
- The Open Library ID: OL15547010M
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.
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26Progress toward national aeronautics goals
By Carlo J. Russo
“Progress toward national aeronautics goals” Metadata:
- Title: ➤ Progress toward national aeronautics goals
- Author: Carlo J. Russo
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Progress toward national aeronautics goals” Subjects and Themes:
- Subjects: Supersonic aircraft - Propulsion - Air breathing engines - General aviation aircraft - Technology transfer
Edition Identifiers:
- The Open Library ID: OL15557176M
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.
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27Interactive calculation procedures for mixed compression inlets
By Eli Reshotko
“Interactive calculation procedures for mixed compression inlets” Metadata:
- Title: ➤ Interactive calculation procedures for mixed compression inlets
- Author: Eli Reshotko
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, School of Engineering, Case Institute of Technology, Case Western Reserve University
- Publish Date: 1983
- Publish Location: Cleveland, Ohio
“Interactive calculation procedures for mixed compression inlets” Subjects and Themes:
- Subjects: ➤ Supersonic aircraft - Laminar boundary layer - Turbulent boundary layer - Shock wave interaction - Oblique shock waves - Nacelles
Edition Identifiers:
- The Open Library ID: OL16125496M
Access and General Info:
- First Year Published: 1983
- 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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28Reaktivnye samolety
“Reaktivnye samolety” Metadata:
- Title: Reaktivnye samolety
- Language: rus
- Number of Pages: Median: 334
- Publisher: AST
- Publish Date: 2000
- Publish Location: Moskva
“Reaktivnye samolety” Subjects and Themes:
- Subjects: SUPERSONIC AIRCRAFT - AIRCRAFT - FIGHTER PLANES - REFERENCE MATERIALS
Edition Identifiers:
- The Open Library ID: OL27050885M
- Online Computer Library Center (OCLC) ID: 79851532
- All ISBNs: 9785237052671 - 5237052673
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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29X-15
By Robert Godwin
“X-15” Metadata:
- Title: X-15
- Author: Robert Godwin
- Language: English
- Number of Pages: Median: 408
- Publisher: Apogee Books
- Publish Date: 2000
- Publish Location: Burlington, Ont
“X-15” Subjects and Themes:
- Subjects: ➤ SUPERSONIC AIRCRAFT - X-15 (Rocket aircraft) - Reusable space vehicles - Hypersonic planes - XLR-99 ENGINE - Research aircraft - RESEARCH VEHICLES - Rocket planes - Winged spacecraft
- Places: United States
Edition Identifiers:
- The Open Library ID: OL3753666M
- Online Computer Library Center (OCLC) ID: 45858759
- Library of Congress Control Number (LCCN): 2003446148
- All ISBNs: 9781896522654 - 1896522653
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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30Turbulence model comparisons for a high-speed aircraft
By Melissa B. Rivers
“Turbulence model comparisons for a high-speed aircraft” Metadata:
- Title: ➤ Turbulence model comparisons for a high-speed aircraft
- Author: Melissa B. Rivers
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information - National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: ➤ Hanover, MD - Springfield, VA - Hampton, Va
“Turbulence model comparisons for a high-speed aircraft” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Supersonic aircraft - Computational grids - Turbulence models - Appication programs (Computers) - Navier-Stokes equation - Transonic wind tunnels - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15569335M
- Online Computer Library Center (OCLC) ID: 44441215
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.
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
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
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
List of supersonic aircraft
A supersonic aircraft is an aircraft which can exceed the speed of sound (Mach 1.0) in level flight. List of aircraft Supersonic aircraft Sound barrier
Supersonic speed
aircraft are supersonic aircraft. No modern-day passenger aircraft are capable of supersonic speed, but there have been supersonic passenger aircraft
Sonic boom
of a supersonic bullet passing overhead or the crack of a bullwhip are examples of a small sonic boom. Sonic booms due to large supersonic aircraft can
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
Supercruise
Supercruise is sustained supersonic flight of a supersonic aircraft without using afterburner. Many supersonic military aircraft are not capable of supercruise
Lockheed Martin X-59 Quesst
Martin X-59 Quesst ("Quiet SuperSonic Technology"), sometimes styled QueSST, is an American experimental supersonic aircraft under development by Skunk
SAI Quiet Supersonic Transport
Quiet Supersonic Transport (QSST) was a project by Supersonic Aerospace International (SAI) to develop a "virtually boomless" commercial supersonic business
Concorde
is a retired Anglo-French supersonic airliner jointly developed and manufactured by Sud Aviation and the British Aircraft Corporation (BAC). Studies