Explore: Subsonic Speed
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Source: The Open Library
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1Cavity unsteady-pressure measurements at subsonic and transonic speeds
By Maureen B. Tracy
“Cavity unsteady-pressure measurements at subsonic and transonic speeds” Metadata:
- Title: ➤ Cavity unsteady-pressure measurements at subsonic and transonic speeds
- Author: Maureen B. Tracy
- Language: English
- Number of Pages: Median: 72
- Publisher: ➤ National Technical Information Service, distributor - Available from National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Cavity unsteady-pressure measurements at subsonic and transonic speeds” Subjects and Themes:
- Subjects: ➤ Cavitation - Cavity flow - Cavity resonators - Measurement - Pressure - Pressure measurement - Subsonic speed - Transonic Aerodynamics - Transonic speed - Unsteady flow - Unsteady flow (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL17135029M - OL17591846M - OL15548837M - OL19158930M - OL18134951M
- Online Computer Library Center (OCLC) ID: 42677336
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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2Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
By W. Pelham Phillips
“Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” Metadata:
- Title: ➤ Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration
- Author: W. Pelham Phillips
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration” Subjects and Themes:
- Subjects: ➤ Spacecraft configurations - Controllability - Supersonic speed - Subsonic speed - Aerodynamic characteristics - Single stage to orbit vehicles - Longitudinal stability - Hypersonics
Edition Identifiers:
- The Open Library ID: OL17516416M - OL17121322M - OL18100856M - OL17687502M
- Online Computer Library Center (OCLC) ID: 38290177
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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3Validation of vortex-lattice method for loads on wings in lift-generated wakes
By Vernon J. Rossow
“Validation of vortex-lattice method for loads on wings in lift-generated wakes” Metadata:
- Title: ➤ Validation of vortex-lattice method for loads on wings in lift-generated wakes
- Author: Vernon J. Rossow
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Washington, DC
“Validation of vortex-lattice method for loads on wings in lift-generated wakes” Subjects and Themes:
- Subjects: ➤ Force distribution - Lift - Loads (Forces) - Rolling moments - Subsonic speed - Vortex lattice method - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17594006M - OL15507839M - OL17126890M - OL18122121M
- Online Computer Library Center (OCLC) ID: 40348464
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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4Low-speed wind tunnel tests of two waverider configuration models
By Robert J. Pegg
“Low-speed wind tunnel tests of two waverider configuration models” Metadata:
- Title: ➤ Low-speed wind tunnel tests of two waverider configuration models
- Author: Robert J. Pegg
- 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, D.C - Springfield, Va
“Low-speed wind tunnel tests of two waverider configuration models” Subjects and Themes:
- Subjects: ➤ Flight characteristics - Directional stability - Lift drag ratio - Wind tunnel tests - Aircraft configurations - Subsonic speed - Aerodynamic stability - Angle of attack - Pitching moments - Waveriders - Lateral stability - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17565252M - OL18118663M - OL15498353M - OL17124624M
- Online Computer Library Center (OCLC) ID: 39554715
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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5A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines
By Wu, Chung-hua.
“A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines” Metadata:
- Title: ➤ A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines
- Author: Wu, Chung-hua.
- 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
“A general theory of two-and three-dimensional rotational flow in subsonic and transonic turbomachines” Subjects and Themes:
- Subjects: ➤ Axial flow - Compressor rotors - Radial flow - Subsonic speed - Three dimensional flow - Transonic compressors - Transonic flow - Turbomachinery - Two dimensional flow - Vortices
Edition Identifiers:
- The Open Library ID: OL15413611M - OL18081145M
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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6Ultra-high bypass ratio jet noise
By Low, John, K. C.
“Ultra-high bypass ratio jet noise” Metadata:
- Title: ➤ Ultra-high bypass ratio jet noise
- Author: Low, John, K. C.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Ultra-high bypass ratio jet noise” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Exhaust nozzles - Wind tunnel tests - Nozzle geometry - Subsonic speed - Bypass ratio - Noise intensity - Noise prediction (Aircraft) - Noise reduction - Jet aircraft noise
Edition Identifiers:
- The Open Library ID: OL17683438M - OL17005197M - OL18078597M
- Online Computer Library Center (OCLC) ID: 32662654
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study
By C. Frederic Smith
“Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study” Metadata:
- Title: ➤ Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study
- Author: C. Frederic Smith
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Lewis Research Center
- Publish Date: 1994
- Publish Location: ➤ [Cleveland, Ohio] - Springfield, Va - [Washington, DC
“Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study” Subjects and Themes:
- Subjects: ➤ Angle of attack - F-18 aircraft - Highly maneuverable aircraft - Inlet airframe configurations - Inlet flow - Research vehicles - Subsonic speed - Vortices
Edition Identifiers:
- The Open Library ID: OL17000516M - OL18075553M - OL15401957M
- Online Computer Library Center (OCLC) ID: 32062761
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Design of supersonic transport flap systems for thrust recovery at subsonic speeds
By Michael J. Mann
“Design of supersonic transport flap systems for thrust recovery at subsonic speeds” Metadata:
- Title: ➤ Design of supersonic transport flap systems for thrust recovery at subsonic speeds
- Author: Michael J. Mann
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Design of supersonic transport flap systems for thrust recovery at subsonic speeds” Subjects and Themes:
- Subjects: Aerodynamic configurations - Design analysis - Flapping - Subsonic speed - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15577761M - OL17597452M
- Online Computer Library Center (OCLC) ID: 45080427
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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9The Kirchhoff formulas for moving surfaces in aeroacoustics
By F. Farassat
“The Kirchhoff formulas for moving surfaces in aeroacoustics” Metadata:
- Title: ➤ The Kirchhoff formulas for moving surfaces in aeroacoustics
- Author: F. Farassat
- 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
“The Kirchhoff formulas for moving surfaces in aeroacoustics” Subjects and Themes:
- Subjects: ➤ Kirchhoff law - Aeroacoustics - Noise prediction - Supersonic flow - Electromagnetism - Subsonic speed - Pipe flow
Edition Identifiers:
- The Open Library ID: OL17807035M - OL15482768M
- Online Computer Library Center (OCLC) ID: 37955730
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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10Study of potential aerodynamic benefits from spanwise blowing at wingtip
By Raymond E. Mineck
“Study of potential aerodynamic benefits from spanwise blowing at wingtip” Metadata:
- Title: ➤ Study of potential aerodynamic benefits from spanwise blowing at wingtip
- Author: Raymond E. Mineck
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Study of potential aerodynamic benefits from spanwise blowing at wingtip” Subjects and Themes:
- Subjects: ➤ Aerodynamic drag - Aerodynamics - Commercial aircraft - Lift - Navier-Stokes equation - Spanwise blowing - Subsonic speed - Swept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15413573M - OL17791713M
- Online Computer Library Center (OCLC) ID: 33401866
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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11Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
By Zachary T. Applin
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Metadata:
- Title: ➤ Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
- Author: Zachary T. Applin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Airfoil profiles - Dynamic pressure - Free flow - Pressure distribution - Semispan models - Subsonic speed - Unswept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15421506M - OL17794166M
- Online Computer Library Center (OCLC) ID: 35231688
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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12Noise impact of advanced high lift systems
By Kevin R. Elmer
“Noise impact of advanced high lift systems” Metadata:
- Title: ➤ Noise impact of advanced high lift systems
- Author: Kevin R. Elmer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Noise impact of advanced high lift systems” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aerodynamic noise - Aircraft design - Engine noise - Jet aircraft noise - Lift - Noise reduction - Passenger aircraft - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL15416073M - OL17791319M
- Online Computer Library Center (OCLC) ID: 33241385
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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13Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
By John E. Lamar
“Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds” Metadata:
- Title: ➤ Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds
- Author: John E. Lamar
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hanover MD - Hampton, Va
“Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamic characteristics - Computational fluid dynamics - Subsonic speed - Transonic speed - Wind tunnel tests - Wing profiles - Geometry - Flight tests - Data integration
Edition Identifiers:
- The Open Library ID: OL17610253M
- Online Computer Library Center (OCLC) ID: 51617379
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack
By Kevin R. Walsh
“Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack” Metadata:
- Title: ➤ Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack
- Author: Kevin R. Walsh
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ̊angle of attack” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - F-18 aircraft - Pressure recovery - Angle of attack - Subsonic speed - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17837959M
- Online Computer Library Center (OCLC) ID: 40617089
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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15Noise exposure reduction of advanced high-lift systems
By Stephen W. Haffner
“Noise exposure reduction of advanced high-lift systems” Metadata:
- Title: ➤ Noise exposure reduction of advanced high-lift systems
- Author: Stephen W. Haffner
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Noise exposure reduction of advanced high-lift systems” Subjects and Themes:
- Subjects: ➤ Aircraft noise - Lift - Aeroacoustics - Aerodynamic noise - Noise reduction - Lift drag ratio - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL15413660M
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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16Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
By Dennis O. Allison
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Metadata:
- Title: ➤ Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
- Author: Dennis O. Allison
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service (NTIS) [distributor
- Publish Date: 1995
- Publish Location: Springfield, VA - Hampton, Va
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Wind tunnel tests - Aircraft models - Subsonic speed - Transonic speed - Maneuverability - Trailing edges - Airfoils - Wing-fuselage stores - Leading edges
Edition Identifiers:
- The Open Library ID: OL15413576M
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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17Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility
By Peter F. Jacobs
“Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility” Metadata:
- Title: ➤ Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility
- Author: Peter F. Jacobs
- Language: English
- Number of Pages: Median: 67
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: [Washington, D.C.]
“Longitudinal aerodynamic characteristics of a subsonic, energy-efficient transport configuration in the National Transonic Facility” Subjects and Themes:
- Subjects: ➤ Transport planes - Nonadiabatic conditions - Longitudinal stability - Subsonic speed - Wall temperature - Boundary layer transition - Aeroelasticity - Supercritical wings
Edition Identifiers:
- The Open Library ID: OL16135206M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Flow unsteadiness effects on boundary layers
By Sreedhara V. Murthy
“Flow unsteadiness effects on boundary layers” Metadata:
- Title: ➤ Flow unsteadiness effects on boundary layers
- Author: Sreedhara V. Murthy
- Language: English
- Publisher: NASA Ames Research Center
- Publish Date: 1989
- Publish Location: [Moffett Field, Calif
“Flow unsteadiness effects on boundary layers” Subjects and Themes:
- Subjects: ➤ Boundary layer transition - Boundary layers - Data bases - Databases - Subsonic speed - Transonic speed - Wind tunnel calibration - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16125542M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Static performance of six innovative thrust reverser concepts for subsonic transport applications
By Scott C. Asbury
“Static performance of six innovative thrust reverser concepts for subsonic transport applications” Metadata:
- Title: ➤ Static performance of six innovative thrust reverser concepts for subsonic transport applications
- Author: Scott C. Asbury
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2000
- Publish Location: Hampton, Va - Hanover, MD
“Static performance of six innovative thrust reverser concepts for subsonic transport applications” Subjects and Themes:
- Subjects: ➤ Turbofans - Aeronautical engineering - Brakes (For arresting motion) - Aircraft brakes - Subsonic speed - Thrust reversal - Performance tests - Aircraft design
Edition Identifiers:
- The Open Library ID: OL16024667M
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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20On the use of controls for subsonic transport performance improvement
By Glenn B. Gilyard
“On the use of controls for subsonic transport performance improvement” Metadata:
- Title: ➤ On the use of controls for subsonic transport performance improvement
- Author: Glenn B. Gilyard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“On the use of controls for subsonic transport performance improvement” Subjects and Themes:
- Subjects: ➤ Aircraft performance - F-15 aircraft - Control systems design - Aircraft control - Subsonic speed - Adaptive control - Optimal control - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL15404387M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
By Julio Chu
“Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Metadata:
- Title: ➤ Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges
- Author: Julio Chu
- 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
“Experimental surface pressure data obtained on 65 ̊delta wing across Reynolds number and Mach number ranges” Subjects and Themes:
- Subjects: ➤ Vortices - Pressure distribution - Wind tunnel tests - Subsonic speed - Slender wings - Reynolds number - Delta wings - Leading edges - Mach number
Edition Identifiers:
- The Open Library ID: OL15504600M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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22Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds
By Julio Chu
“Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds” Metadata:
- Title: ➤ Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds
- Author: Julio Chu
- Number of Pages: Median: 238
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Pressure meaurements on a thick cambered and twisted 58 [degree] delta wing at high subsonic speeds” Subjects and Themes:
- Subjects: Delta wings - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL19247966M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils
By Daryl Lawrence Bonhaus
“Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils” Metadata:
- Title: ➤ Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils
- Author: Daryl Lawrence Bonhaus
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Numerical study to assess sulfur hexafluoride as a medium for testing multielement airfoils” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Galerkin method - Viscous flow - Sulfur hexafluoride - Unstructured grids (Mathematics) - Subsonic speed - Navier-Stokes equation - Airfoil profiles - Wind tunnel tests - Runge-Kutta method
Edition Identifiers:
- The Open Library ID: OL15413571M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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24Highlights of aeroacoustics research in the U.S.-1998
By Ganesh Raman
“Highlights of aeroacoustics research in the U.S.-1998” Metadata:
- Title: ➤ Highlights of aeroacoustics research in the U.S.-1998
- Author: Ganesh Raman
- 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
“Highlights of aeroacoustics research in the U.S.-1998” Subjects and Themes:
- Subjects: Progress - Rotary wing aircraft - Aeroacoustics - Subsonic speed - Research
Edition Identifiers:
- The Open Library ID: OL15550659M
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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25Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
By A. M. Springer
“Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” Metadata:
- Title: ➤ Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept
- Author: A. M. Springer
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Marshall Space Flight Center
- Publish Date: 1995
- Publish Location: [Springfield, Va - MSFC, Ala
“Transonic aerodynamic characteristics of a proposed wing-body reusable launch vehicle concept” Subjects and Themes:
- Subjects: ➤ Body-wing configurations - Aerodynamic characteristics - Wind tunnel tests - Longitudinal stability - Subsonic speed - Aerodynamic stability - Angle of attack - Single stage to orbit vehicles - Sideslip - Aerodynamic forces - Lateral stability - Control surfaces - Transonic speed - Mach number - Spacecraft stability
Edition Identifiers:
- The Open Library ID: OL15416729M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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26Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory
By E. Carson Yates
“Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory” Metadata:
- Title: ➤ Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory
- Author: E. Carson Yates
- Language: English
- Number of Pages: Median: 16
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va - [Springfield, Va
“Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory” Subjects and Themes:
- Subjects: ➤ Surfaces - Lift - Aerodynamic coefficients - Unsteady flow - Aerodynamics - Sensitivity - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL15409051M
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:
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27The development of a highly reliable power management and distribution system for civil transport aircraft
By Anthony S. Coleman
“The development of a highly reliable power management and distribution system for civil transport aircraft” Metadata:
- Title: ➤ The development of a highly reliable power management and distribution system for civil transport aircraft
- Author: Anthony S. Coleman
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“The development of a highly reliable power management and distribution system for civil transport aircraft” Subjects and Themes:
- Subjects: ➤ Avionics - Transport aircraft - Pneumatics - Actuators - Fly by wire control - Subsonic speed - Flight control - Management systems - Reliability - Rudders - Hydraulic equipment - Wings - Electromagnetic interference
Edition Identifiers:
- The Open Library ID: OL15403788M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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28Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions
By Richard P. Woodward
“Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions” Metadata:
- Title: ➤ Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions
- Author: Richard P. Woodward
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions” Subjects and Themes:
- Subjects: ➤ Tip speed - Propeller fans - Noise measurement - Subsonic speed - Counter rotation - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15406047M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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29Subsonic dynamics of stardust sample return capsule
By R. A. Mitcheltree
“Subsonic dynamics of stardust sample return capsule” Metadata:
- Title: ➤ Subsonic dynamics of stardust sample return capsule
- Author: R. A. Mitcheltree
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: Hampton, Va - [Springfield, Va
“Subsonic dynamics of stardust sample return capsule” Subjects and Themes:
- Subjects: ➤ Landing modules - Aerodynamics - Wind tunnel tests - Subsonic speed - Dynamic stability - Space capsules - Stability tests - Atmospheric entry
Edition Identifiers:
- The Open Library ID: OL15482780M
Access and General Info:
- First Year Published: 1997
- 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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30Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
“Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft” Metadata:
- Title: ➤ Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1999
- Publish Location: ➤ Edwards, Calif - Springfield, VA
“Factors affecting inlet-engine compatibility during aircraft departures at high angle of attack for an F/A-18A aircraft” Subjects and Themes:
- Subjects: ➤ F-18 aircraft - Compressors - Subsonic speed - Aerodynamic stability - Angle of attack - Flight control - Research vehicles - Rotors - Control surfaces
Edition Identifiers:
- The Open Library ID: OL17839405M
- Online Computer Library Center (OCLC) ID: 41964667
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:
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