Explore: Nozzle Geometry
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Two-dimensional converging-diverging rippled nozzles at transonic speeds
By John R. Carlson
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Metadata:
- Title: ➤ Two-dimensional converging-diverging rippled nozzles at transonic speeds
- Author: John R. Carlson
- Language: English
- Number of Pages: Median: 105
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Subjects and Themes:
- Subjects: ➤ Convergent-divergent nozzles - Discharge coefficient - Drag - Nozzle flow - Nozzle geometry - Nozzles - Ripples - Thrust - Trailing edges - Transonic speed - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: ➤ OL19752932M - OL16487219M - OL15403665M - OL16982124M - OL19753709M - OL18076297M
- Online Computer Library Center (OCLC) ID: 32220800
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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2Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes
By Robert J. Foley
“Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes” Metadata:
- Title: ➤ Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes
- Author: Robert J. Foley
- Language: English
- Number of Pages: Median: 77
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service - Langley Research Center
- Publish Date: 1991
- Publish Location: ➤ Washington, D.C - Hampton, Va - Springfield, Va
“Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes” Subjects and Themes:
- Subjects: ➤ Thrust vector control - Testing - Jet vanes - Motors - Yaw - Static tests - Yawing (Aerodynamics) - Blades - Jet nozzles - Nozzle geometry - Airplanes - Thrust - Static thrust - Convergent-divergent nozzles - Yaw vanes - Nozzles
Edition Identifiers:
- The Open Library ID: OL17723834M - OL18214753M - OL20420347M - OL19166080M
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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3CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system
By Ing Chuang
“CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system” Metadata:
- Title: ➤ CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system
- Author: Ing Chuang
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Computational fluid dynamics - Turbojet engines - Engine design - Nozzle geometry - Hypersonic flight - Nozzle thrust coefficients - Flow distribution - Ramjet engines - Nozzle walls
Edition Identifiers:
- The Open Library ID: OL18120912M - OL17593566M - OL15503241M - OL17134628M
- Online Computer Library Center (OCLC) ID: 42555294
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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4Ultra-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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5Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows
By Scott T. Imlay
“Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” Metadata:
- Title: ➤ Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows
- Author: Scott T. Imlay
- Language: English
- Number of Pages: Median: 180
- Publisher: ➤ Langley Research Center - 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 - Hampton, Va - [Washington, D.C.]
“Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows” Subjects and Themes:
- Subjects: ➤ Thrust vector control - Finite volume method - Navier-Stokes equation - Thrust reversal - Nozzle flow - Time marching - Computational fluid dynamics - Flow equations - Airplanes - Nozzle geometry - Nozzles - Convergent-divergent nozzles - Numerical solutions - Navier-Stokes equations - Motors
Edition Identifiers:
- The Open Library ID: OL18083141M - OL15417264M - OL20986195M
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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6Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
By Robert S. Jankovsky
“Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure” Metadata:
- Title: ➤ Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
- Author: Robert S. Jankovsky
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure” Subjects and Themes:
- Subjects: ➤ Thrust chamber pressure - Exhaust velocity - Divergent nozzles - Specific impulse - Nozzle geometry - Nozzle thrust coefficients - Nozzle efficiency - Rocket nozzles
Edition Identifiers:
- The Open Library ID: OL17126935M - OL17697710M - OL17838890M
- Online Computer Library Center (OCLC) ID: 40386575
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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7Computing axisymmetric jet screech tones using unstructured grids
By Philip C. E. Jorgenson
“Computing axisymmetric jet screech tones using unstructured grids” Metadata:
- Title: ➤ Computing axisymmetric jet screech tones using unstructured grids
- Author: Philip C. E. Jorgenson
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Glenn Research Center - Available from the NASA Center for Aerospace Information
- Publish Date: 2002
- Publish Location: ➤ Hanover, MD - [Cleveland, Ohio] - Springfield, VA
“Computing axisymmetric jet screech tones using unstructured grids” Subjects and Themes:
- Subjects: Aeroacoustics - Axisymmetric flow - Nozzle geometry - Screech tones - Unstructured grids
Edition Identifiers:
- The Open Library ID: OL17634848M - OL16098758M
- Online Computer Library Center (OCLC) ID: 57252947
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Investigation of ramp injectors for supersonic mixing enhancement
By Y. Haimovitch
“Investigation of ramp injectors for supersonic mixing enhancement” Metadata:
- Title: ➤ Investigation of ramp injectors for supersonic mixing enhancement
- Author: Y. Haimovitch
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: [Springfield, VA - Hampton, Va
“Investigation of ramp injectors for supersonic mixing enhancement” Subjects and Themes:
- Subjects: ➤ Nozzle inserts - Fuel injection - Supersonic flow - Nozzle geometry - Supersonic combustion ramjet engines - Turbulent mixing - Spray nozzles - Wind tunnel tests - Injectors
Edition Identifiers:
- The Open Library ID: OL15409145M - OL17790638M
- Online Computer Library Center (OCLC) ID: 32712612
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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9Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air
By W. I. Scallion
“Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air” Metadata:
- Title: ➤ Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air
- Author: W. I. Scallion
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1991
- Publish Location: Hamtpon, Va - [Springfield, Va
“Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air” Subjects and Themes:
- Subjects: ➤ Shapes - Nozzle design - Pressure ratio - Supersonic nozzles - Plumes - Nozzle geometry
Edition Identifiers:
- The Open Library ID: OL17634727M - OL16124008M
- Online Computer Library Center (OCLC) ID: 59760125
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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10Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers
By Robert J. Boyle
“Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers” Metadata:
- Title: ➤ Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers
- Author: Robert J. Boyle
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Heat transfer predictions for two turbine nozzle geometries at high Reynolds and Mach numbers” Subjects and Themes:
- Subjects: ➤ Aerodynamic heat transfer - Computational fluid dynamics - Guide vanes - High Reynolds number - Nozzle geometry - Transonic flow - Turbines - Turbulence models
Edition Identifiers:
- The Open Library ID: OL15420804M - OL17794624M
- Online Computer Library Center (OCLC) ID: 34779799
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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11The effects of magnetic nozzle configurations on plasma thrusters
By Peter J. Turchi
“The effects of magnetic nozzle configurations on plasma thrusters” Metadata:
- Title: ➤ The effects of magnetic nozzle configurations on plasma thrusters
- Author: Peter J. Turchi
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“The effects of magnetic nozzle configurations on plasma thrusters” Subjects and Themes:
- Subjects: ➤ Electric propulsion - Electric rocket engines - Magnetoplasmadynamics - Nozzle geometry - Plasma engines - Rocket engines
Edition Identifiers:
- The Open Library ID: OL15507242M
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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12Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case
By Joseph F. Baumeister
“Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case” Metadata:
- Title: ➤ Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case
- Author: Joseph F. Baumeister
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Radiant energy measurements from a scaled jet engine axisymmetric exhaust nozzle for a baseline code validation case” Subjects and Themes:
- Subjects: ➤ Jet engines - Exhaust nozzles - Computer programs - Thermal analysis - Nozzle geometry - Radiation measurement - Aircraft engines
Edition Identifiers:
- The Open Library ID: OL15403957M
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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13Screech tones of supersonic jets from bevelled rectangular nozzles
By Christopher K. W. Tam
“Screech tones of supersonic jets from bevelled rectangular nozzles” Metadata:
- Title: ➤ Screech tones of supersonic jets from bevelled rectangular nozzles
- Author: Christopher K. W. Tam
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Reston, VA - [Washington, DC - Springfield, Va
“Screech tones of supersonic jets from bevelled rectangular nozzles” Subjects and Themes:
- Subjects: ➤ Boundary value problems - Finite difference theory - Mach number - Nozzle geometry - Supersonic jet flow - Supersonic nozzles - Wave guides - Waveguides
Edition Identifiers:
- The Open Library ID: OL15494983M
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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14An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct
By Bruce A. Reichert
“An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct” Metadata:
- Title: ➤ An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct
- Author: Bruce A. Reichert
- Language: English
- Publisher: Lewis Research Center
- Publish Date: 1991
- Publish Location: [Cleveland, Ohio
“An experimental comparison of nonswirling and swirling flow in a circular-to-rectangular transition duct” Subjects and Themes:
- Subjects: ➤ Ducts - Swirling - Flow geometry - Exhaust nozzles - Nozzle geometry - Ducted flow
Edition Identifiers:
- The Open Library ID: OL16126995M
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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15Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
By George T. Carson
“Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20” Metadata:
- Title: ➤ Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
- Author: George T. Carson
- Language: English
- Number of Pages: Median: 171
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Division
- Publish Date: 1988
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20” Subjects and Themes:
- Subjects: ➤ Ramjet engines - Nozzle efficiency - Turbine engines - Jet nozzles - Rocket nozzles - Nozzle geometry - Mach number
Edition Identifiers:
- The Open Library ID: OL16116426M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept
By David J. Wing
“Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept” Metadata:
- Title: ➤ Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept
- Author: David J. Wing
- 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
“Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept” Subjects and Themes:
- Subjects: ➤ Testing - Sonic nozzles - Exhaust nozzles - Jet nozzles - Wind tunnel tests - Nozzle geometry - Static tests - Throats - Skewness - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL17000202M
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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17Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
By David J. Wing
“Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct” Metadata:
- Title: ➤ Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
- Author: David J. Wing
- 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
“Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct” Subjects and Themes:
- Subjects: ➤ Pitch (Inclination) - Convergent nozzles - Flapping - Angular distribution - Thrust vector control - Nozzle geometry - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15542756M
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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18Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle
By Ganesh Raman
“Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle” Metadata:
- Title: ➤ Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle
- Author: Ganesh Raman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Nozzle geometry - Jet aircraft noise - Aerodynamic characteristics - Aircraft engines - Thrust augmentation - Engine noise - Acoustic properties
Edition Identifiers:
- The Open Library ID: OL15504879M
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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19Analysis and design of optimized truncated scarfed nozzles subject to external flow effects
By Rickey J. Shyne
“Analysis and design of optimized truncated scarfed nozzles subject to external flow effects” Metadata:
- Title: ➤ Analysis and design of optimized truncated scarfed nozzles subject to external flow effects
- Author: Rickey J. Shyne
- Language: English
- Number of Pages: Median: 10
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Analysis and design of optimized truncated scarfed nozzles subject to external flow effects” Subjects and Themes:
- Subjects: ➤ Nozzles - Nozzle design - Ramjet engines - Exhaust nozzles - Nozzle geometry - Airplanes - Flow distribution
Edition Identifiers:
- The Open Library ID: OL16132137M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Decomposing solid micropropulsion nozzle performance issues
By Brian D. Reed
“Decomposing solid micropropulsion nozzle performance issues” Metadata:
- Title: ➤ Decomposing solid micropropulsion nozzle performance issues
- Author: Brian D. Reed
- Language: English
- Publisher: ➤ Available from the NASA Center for Aerospace Information - National Technical Information Service [distributor - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: ➤ Springfield, VA - [Cleveland, Ohio] - Hanover, MD
“Decomposing solid micropropulsion nozzle performance issues” Subjects and Themes:
- Subjects: ➤ Solid propellants - Nozzle design - Spacecraft propulsion - Nozzle efficiency - Nozzle geometry - Thrustors - Miniaturization
Edition Identifiers:
- The Open Library ID: OL16098336M
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
By Kenneth J. Davidian
“A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center” Metadata:
- Title: ➤ A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
- Author: Kenneth J. Davidian
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.?]
“A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center” Subjects and Themes:
- Subjects: ➤ Nozzles - Rockets (Aeronautics) - Rocket nozzles - Nozzle geometry - High aspect ratio - Research facilities
Edition Identifiers:
- The Open Library ID: OL15419235M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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22Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap
By Richard J. Re
“Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap” Metadata:
- Title: ➤ Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap
- Author: Richard J. Re
- 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: ➤ [Washington, D.C.] - Springfield, Va
“Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap” Subjects and Themes:
- Subjects: ➤ Jet planes - Thrust vector control - Jet nozzles - Wind tunnel tests - Nozzle geometry - Static tests - Thrust reversal - Transonic wind tunnels - Thrust reversers
Edition Identifiers:
- The Open Library ID: OL16116655M
Access and General Info:
- First Year Published: 1986
- 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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23Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
By Mary L. Mason
“Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability” Metadata:
- Title: ➤ Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability
- Author: Mary L. Mason
- 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.]
“Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability” Subjects and Themes:
- Subjects: ➤ Axisymmetric flow - Pitching (Aerodynamics) - Thrust vector control - Motors - Nozzle geometry - Airplanes - Short takeoff aircraft - Short take-off and landing aircraft - Static tests - Testing - Nozzle thrust coefficients - Jet nozzles - Thrust
Edition Identifiers:
- The Open Library ID: OL16116664M
Access and General Info:
- First Year Published: 1986
- 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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24Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle
By David W. Lam
“Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle” Metadata:
- Title: ➤ Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle
- Author: David W. Lam
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Use of the PARC code to estimate the off-design transonic performance of an over/under turboramjet nozzle” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Navier-Stokes equation - Transonic flow - Nozzle geometry - Turboramjet engines - Nozzle efficiency - Nozzle flow - Hypersonic nozzles - Nozzle design
Edition Identifiers:
- The Open Library ID: OL15414400M
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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25Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility
By Kin C. Wong
“Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility” Metadata:
- Title: ➤ Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility
- Author: Kin C. Wong
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from the NASA Center for Aerospace Information
- Publish Date: 2003
- Publish Location: ➤ [Cleveland, Ohio] - [Hanover, Md
“Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility” Subjects and Themes:
- Subjects: ➤ Test facilities - Thrust measurement - Exhaust nozzles - Calibrating - Nozzle geometry - Data reduction - Axial loads
Edition Identifiers:
- The Open Library ID: OL16098340M
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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26Space shuttle ice suppression system validation
By J. L. F. Porteiro
“Space shuttle ice suppression system validation” Metadata:
- Title: ➤ Space shuttle ice suppression system validation
- Author: J. L. F. Porteiro
- Language: English
- Publisher: ➤ Texas Engineering Experiment Station, Texas A&M University
- Publish Date: 1983
- Publish Location: College Station, Tex
“Space shuttle ice suppression system validation” Subjects and Themes:
- Subjects: Ice prevention - Space shuttles - Nozzle geometry
Edition Identifiers:
- The Open Library ID: OL16116885M
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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