Explore: Jet Nozzles
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles
By P. D. Thomas
“Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles” Metadata:
- Title: ➤ Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles
- Author: P. D. Thomas
- Language: English
- Number of Pages: Median: 111
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1979 - 1980
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Numerical method for predicting flow characteristics and performance of nonaxisymmetric nozzles” Subjects and Themes:
- Subjects: Nozzles - Jet nozzles - Fluid dynamics - Navier-Stokes equations
Edition Identifiers:
- The Open Library ID: ➤ OL17823784M - OL14930501M - OL17823157M - OL17652264M - OL17651798M - OL14930320M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Boundary-layer separation on isolated boattail nozzles
By William Kelly Abeyounis
“Boundary-layer separation on isolated boattail nozzles” Metadata:
- Title: ➤ Boundary-layer separation on isolated boattail nozzles
- Author: William Kelly Abeyounis
- Language: English
- Number of Pages: Median: 60
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1978
- Publish Location: Washington - Springfield, Va
“Boundary-layer separation on isolated boattail nozzles” Subjects and Themes:
- Subjects: Jet nozzles - Airplanes - Laminar flow - Nacelles
Edition Identifiers:
- The Open Library ID: OL18014163M - OL17537910M - OL14932061M - OL15227214M - OL17979077M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
By Laurence D. Leavitt
“Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics” Metadata:
- Title: ➤ Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics
- Author: Laurence D. Leavitt
- Language: English
- Number of Pages: Median: 103
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1983
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Effects of twin-vertical-tail parameters on twin-engine afterbody/nozzle aerodynamic characteristics” Subjects and Themes:
- Subjects: Fighter planes - Jet nozzles - Tail surfaces - Flight testing
Edition Identifiers:
- The Open Library ID: OL15304223M - OL17553404M - OL18036386M
Author's Alternative Names:
"Laurence D Leavitt"Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Static 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
Online Access
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5Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application
By B. A. Janardan
“Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application” Metadata:
- Title: ➤ Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application
- Author: B. A. Janardan
- Language: English
- Number of Pages: Median: 198
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1984 - 1985
- Publish Location: [Washington, D.C.?]
“Free jet feasibility study of a thermal acoustic shield concept for AST/VCE application” Subjects and Themes:
- Subjects: Jet nozzles
Edition Identifiers:
- The Open Library ID: OL17679966M - OL17831476M - OL14931281M - OL17665863M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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6Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle
By Scott C. Asbury
“Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle” Metadata:
- Title: ➤ Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle
- Author: Scott C. Asbury
- Language: English
- Number of Pages: Median: 107
- Publisher: ➤ National Technical Information Service, distributor] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle” Subjects and Themes:
- Subjects: Jet nozzles - Nozzles - Yaw - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL19917593M - OL15386000M - OL14700565M - OL18064618M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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7Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression
By James R. DeBonis
“Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression” Metadata:
- Title: ➤ Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression
- Author: James R. DeBonis
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1992
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Full Navier-Stokes analysis of a two-dimensional mixer/ejector nozzle for noise suppression” Subjects and Themes:
- Subjects: Jet nozzles - Noise - Airplanes
Edition Identifiers:
- The Open Library ID: OL15364819M - OL16382477M - OL18054787M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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8Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles
By Verlon L. Head
“Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles” Metadata:
- Title: ➤ Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles
- Author: Verlon L. Head
- Language: English
- Number of Pages: Median: 92
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administation, Scientific and Technical Information Office
- Publish Date: 1984
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles” Subjects and Themes:
- Subjects: Testing - Jet nozzles - Turbojet engines - Airplanes
Edition Identifiers:
- The Open Library ID: OL15306037M - OL18036966M - OL17554221M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9User's guide for the NOZL3D and NOZLIC computer programs
By P. D. Thomas
“User's guide for the NOZL3D and NOZLIC computer programs” Metadata:
- Title: ➤ User's guide for the NOZL3D and NOZLIC computer programs
- Author: P. D. Thomas
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1980
- Publish Location: Hampton, Va
“User's guide for the NOZL3D and NOZLIC computer programs” Subjects and Themes:
- Subjects: Jet nozzles - Scientific applications - Numerical solutions - Navier-Stokes equations - Computer programs
Edition Identifiers:
- The Open Library ID: OL14927474M - OL17831778M - OL17666364M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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10Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds
By E. Ann Bare
“Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds” Metadata:
- Title: ➤ Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds
- Author: E. Ann Bare
- Language: English
- Number of Pages: Median: 88
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1983
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Effect of thrust reverser operation on the lateral-directional characteristics of a three-surface F-15 model at transonic speeds” Subjects and Themes:
- Subjects: Jet nozzles - Jet planes - Thrust reversers
Edition Identifiers:
- The Open Library ID: OL17663540M - OL14933459M - OL17830293M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11Evaluation of flip-flop jet nozzles for use as practical excitation devices
By Raman Ganesh
“Evaluation of flip-flop jet nozzles for use as practical excitation devices” Metadata:
- Title: ➤ Evaluation of flip-flop jet nozzles for use as practical excitation devices
- Author: Raman Ganesh
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Evaluation of flip-flop jet nozzles for use as practical excitation devices” Subjects and Themes:
- Subjects: Jet nozzles
Edition Identifiers:
- The Open Library ID: OL17681757M - OL18070941M - OL14666745M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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12Viscous computations of cold air/airflow around scramjet nozzle afterbody
By Oktay Baysal
“Viscous computations of cold air/airflow around scramjet nozzle afterbody” Metadata:
- Title: ➤ Viscous computations of cold air/airflow around scramjet nozzle afterbody
- Author: Oktay Baysal
- Language: English
- Number of Pages: Median: 65
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Viscous computations of cold air/airflow around scramjet nozzle afterbody” Subjects and Themes:
- Subjects: Computational fluid dynamics - Hypersonic Aerodynamics - Hypersonic vehicles - Jet nozzles - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL15372804M - OL21499696M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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13Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement
By Carpenter, Thomas.
“Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement” Metadata:
- Title: ➤ Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement
- Author: Carpenter, Thomas.
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - California Polytechnic State University - National Aeronautics and Space Administration
- Publish Date: 1991 - 1992
- Publish Location: ➤ [Washington, DC - San Luis Obispo, Calif - Springfield, Va
“Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement” Subjects and Themes:
- Subjects: Jet nozzles - Evaluation
Edition Identifiers:
- The Open Library ID: OL15391254M - OL15379677M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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14Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps
By Laurence D. Leavitt
“Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps” Metadata:
- Title: ➤ Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps
- Author: Laurence D. Leavitt
- Language: English
- Number of Pages: Median: 33
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration,Scientific and Technical Information Branch
- Publish Date: 1982
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Performance characteristics of axisymmetric convergent-divergent exhaust nozzles with longitudinal slots in the divergent flaps” Subjects and Themes:
- Subjects: Nozzles - Jet nozzles
Edition Identifiers:
- The Open Library ID: OL17654721M - OL17827738M
Author's Alternative Names:
"Laurence D Leavitt"Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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15Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20
By Francis J Capone
“Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20” Metadata:
- Title: ➤ Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20
- Author: Francis J Capone
- Language: English
- Number of Pages: Median: 188
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration
- Publish Date: 1977
- Publish Location: Washington - Springfield, Va
“Performance of twin-dimensional wedge nozzles including thrust vectoring and reversing effects at speeds up to Mach 2.20” Subjects and Themes:
- Subjects: Jet nozzles - Jet planes - Thrust reversers
Edition Identifiers:
- The Open Library ID: OL17976984M - OL14925086M
Access and General Info:
- First Year Published: 1977
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Jet engine hot parts IR analysis procedure (J-EIRP)
By Joseph F. Baumeister
“Jet engine hot parts IR analysis procedure (J-EIRP)” Metadata:
- Title: ➤ Jet engine hot parts IR analysis procedure (J-EIRP)
- Author: Joseph F. Baumeister
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Jet engine hot parts IR analysis procedure (J-EIRP)” Subjects and Themes:
- Subjects: Jet nozzles - Infrared radiation
Edition Identifiers:
- The Open Library ID: OL14690528M - OL17678065M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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17Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20
By George T. Carson
“Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20” Metadata:
- Title: ➤ Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20
- Author: George T. Carson
- Language: English
- Number of Pages: Median: 123
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1984
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“Aeropropulsive characteristics of nonaxisymmetric-nozzle thrust reversers at Mach numbers from 0 to 1.20” Subjects and Themes:
- Subjects: Jet nozzles
Edition Identifiers:
- The Open Library ID: OL17666396M - OL17831808M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions
By George T. Carson
“Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions” Metadata:
- Title: ➤ Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions
- Author: George T. Carson
- Language: English
- Number of Pages: Median: 42
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - [Washington]
“Experimental and analytical investigation of a nonaxisymmetric and wedge nozzle at static conditions” Subjects and Themes:
- Subjects: Jet nozzles
Edition Identifiers:
- The Open Library ID: OL17647826M - OL17818500M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles
By Verlon L Head
“Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles” Metadata:
- Title: ➤ Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles
- Author: Verlon L Head
- Language: English
- Number of Pages: Median: 92
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1984
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Hot-flow tests of a series of 10-percent-scale turbofan forced mixing nozzles” Subjects and Themes:
- Subjects: Testing - Jet nozzles - Turbojet engines - Airplanes
Edition Identifiers:
- The Open Library ID: OL17979766M - OL14933511M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers
By Odis C. Pendergraft
“Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers” Metadata:
- Title: ➤ Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers
- Author: Odis C. Pendergraft
- Language: English
- Number of Pages: Median: 168
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1982
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers” Subjects and Themes:
- Subjects: Performance - Jet nozzles - Jet planes - Thrust reversers - Airplanes
Edition Identifiers:
- The Open Library ID: OL17655777M - OL17828604M
Author's Alternative Names:
"Odis C Pendergraft"Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement
By Thomas W. Carpenter
“Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement” Metadata:
- Title: ➤ Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement
- Author: Thomas W. Carpenter
- Language: English
- Publisher: ➤ California Polytechnic State University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1991 - 1992
- Publish Location: ➤ Springfield, Va - San Luis Obispo, Calif - [Washington, DC
“Evaluation of dual flow, thrust vector nozzles with exhaust stream impingement” Subjects and Themes:
- Subjects: Jet nozzles - Evaluation
Edition Identifiers:
- The Open Library ID: OL14704229M - OL14696763M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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22Experimental results of a deflected thrust V/STOL nozzle research program
By Paul L. Burstadt
“Experimental results of a deflected thrust V/STOL nozzle research program” Metadata:
- Title: ➤ Experimental results of a deflected thrust V/STOL nozzle research program
- Author: Paul L. Burstadt
- Language: English
- Number of Pages: Median: 24
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1983
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Experimental results of a deflected thrust V/STOL nozzle research program” Subjects and Themes:
- Subjects: Jet nozzles - Coriolis force
Edition Identifiers:
- The Open Library ID: OL17800304M - OL17663040M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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23Viscous three-dimensional analyses for nozzles for hypersonic propulsion
By G. J. Harloff
“Viscous three-dimensional analyses for nozzles for hypersonic propulsion” Metadata:
- Title: ➤ Viscous three-dimensional analyses for nozzles for hypersonic propulsion
- Author: G. J. Harloff
- Language: English
- Publisher: ➤ Sverdrup Technology, Inc., NASA Lewis Research Center Group - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Cleveland, Ohio
“Viscous three-dimensional analyses for nozzles for hypersonic propulsion” Subjects and Themes:
- Subjects: Nozzles - Jet nozzles - Fluid dynamics
Edition Identifiers:
- The Open Library ID: OL15281848M - OL18031103M
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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24Effect of initial tangential velocity distribution on the mean evolution of a swirling turbulent free jet
By Saeed Farokhi
“Effect of initial tangential velocity distribution on the mean evolution of a swirling turbulent free jet” Metadata:
- Title: ➤ Effect of initial tangential velocity distribution on the mean evolution of a swirling turbulent free jet
- Author: Saeed Farokhi
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration
- Publish Date: 1988
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Effect of initial tangential velocity distribution on the mean evolution of a swirling turbulent free jet” Subjects and Themes:
- Subjects: Aerodynamics - Jet nozzles - Turbulence
Edition Identifiers:
- The Open Library ID: OL15278388M
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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25Turbines and jet nozzles with two-phase flows
By V. D. Venediktov
“Turbines and jet nozzles with two-phase flows” Metadata:
- Title: ➤ Turbines and jet nozzles with two-phase flows
- Author: V. D. Venediktov
- Language: English
- Number of Pages: Median: 232
- Publisher: Management Information Service
- Publish Date: 1970
- Publish Location: Detroit, Mich
“Turbines and jet nozzles with two-phase flows” Subjects and Themes:
- Subjects: Jet nozzles - Turbines - Two-phase flow
Edition Identifiers:
- The Open Library ID: OL5701911M
- Library of Congress Control Number (LCCN): 70130609
Access and General Info:
- First Year Published: 1970
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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26Two-phase flow in turbines and reaction nozzles
By V. D. Venediktov
“Two-phase flow in turbines and reaction nozzles” Metadata:
- Title: ➤ Two-phase flow in turbines and reaction nozzles
- Author: V. D. Venediktov
- Language: English
- Number of Pages: Median: 187
- Publisher: ➤ National Aeronautics and Space Administration - National Aeronautics and Space Administration; for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va. - for sale by the Clearinghouse for Federal Scientific and Technical Information
- Publish Date: 1970
- Publish Location: [Washington]
“Two-phase flow in turbines and reaction nozzles” Subjects and Themes:
- Subjects: Jet nozzles - Turbines - Two-phase flow
Edition Identifiers:
- The Open Library ID: OL5738776M
- Online Computer Library Center (OCLC) ID: 106815
- Library of Congress Control Number (LCCN): 70607833
Access and General Info:
- First Year Published: 1970
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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27Studies of flow fields created by vertical and inclined jets when stationary or moving over a horizontal surface
By W. A. Abbott
“Studies of flow fields created by vertical and inclined jets when stationary or moving over a horizontal surface” Metadata:
- Title: ➤ Studies of flow fields created by vertical and inclined jets when stationary or moving over a horizontal surface
- Author: W. A. Abbott
- Language: English
- Number of Pages: Median: 17
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“Studies of flow fields created by vertical and inclined jets when stationary or moving over a horizontal surface” Subjects and Themes:
- Subjects: Jet nozzles - Jet propulsion - Vertically rising aircraft
Edition Identifiers:
- The Open Library ID: OL5580015M
- Library of Congress Control Number (LCCN): 67094050
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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28Viscous flow simulations of internal store carriage and separation
By Oktay Baysal
“Viscous flow simulations of internal store carriage and separation” Metadata:
- Title: ➤ Viscous flow simulations of internal store carriage and separation
- Author: Oktay Baysal
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Dept. of Mechanical Engineering & Mechanics, College of Engineering & Technology, Old Dominion University
- Publish Date: 1991
- Publish Location: [Washington, D.C - Norfolk, Va
“Viscous flow simulations of internal store carriage and separation” Subjects and Themes:
- Subjects: ➤ Airplanes - Computer simulation - Hypersonic Aerodynamics - Jet nozzles - Ramjet engines - Supersonic Aerodynamics - Viscous flow
Edition Identifiers:
- The Open Library ID: OL15382511M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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29Aircraft ground test and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes
By Steven A. Johnson
“Aircraft ground test and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes” Metadata:
- Title: ➤ Aircraft ground test and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes
- Author: Steven A. Johnson
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Aircraft ground test and subscale model results of axial thrust loss caused by thrust vectoring using turning vanes” Subjects and Themes:
- Subjects: Airplanes - Jet nozzles - Motors - Thrust
Edition Identifiers:
- The Open Library ID: OL15363931M
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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30Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability
By Taylor, John G.
“Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability” Metadata:
- Title: ➤ Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability
- Author: Taylor, John G.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Static investigation of a two-dimensional convergent-divergent exhaust nozzle with multiaxis thrust-vectoring capability” Subjects and Themes:
- Subjects: Aircraft exhaust emissions - Jet nozzles
Edition Identifiers:
- The Open Library ID: OL15368336M
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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31Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20
By Odis C. Pendergraft
“Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20” Metadata:
- Title: ➤ Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20
- Author: Odis C. Pendergraft
- Language: English
- Publisher: ➤ National Technical Information Service [distributor] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ [Washington, DC] - [Springfield, Va.?
“Parametric study of afterbody/nozzle drag on twin two-dimensional convergent-divergent nozzles at mach numbers from 0.60 to 1.20” Subjects and Themes:
- Subjects: Jet nozzles - Aerodynamic load
Edition Identifiers:
- The Open Library ID: OL15362829M
Author's Alternative Names:
"Odis C Pendergraft"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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32Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰
By Laurence D. Leavitt
“Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰” Metadata:
- Title: ➤ Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰
- Author: Laurence D. Leavitt
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: [Washington, D.C.]
“Static internal performance of a two-dimensional convergent nozzle with thrust-vectoring capability up to 60⁰” Subjects and Themes:
- Subjects: Jet nozzles - Testing
Edition Identifiers:
- The Open Library ID: OL16114872M
Author's Alternative Names:
"Laurence D Leavitt"Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model
By Francis J Capone
“Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model” Metadata:
- Title: ➤ Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model
- Author: Francis J Capone
- Language: English
- Number of Pages: Median: 77
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1982
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model” Subjects and Themes:
- Subjects: Jet nozzles
Edition Identifiers:
- The Open Library ID: OL14933185M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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34Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft
By Francis J Capone
“Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft” Metadata:
- Title: ➤ Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft
- Author: Francis J Capone
- Language: English
- Number of Pages: Median: 85
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1983
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Effect of thrust vectoring and wing maneuver devices on transonic aeropropulsive characteristics of a supersonic fighter aircraft” Subjects and Themes:
- Subjects: Jet nozzles - Fighter planes
Edition Identifiers:
- The Open Library ID: OL14933303M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35Design and evaluation of single and dual flow thrust vector nozzles with post exit vanes
semi-annual progress report 6/92 - 12/92
By Carpenter, Thomas.
“Design and evaluation of single and dual flow thrust vector nozzles with post exit vanes” Metadata:
- Title: ➤ Design and evaluation of single and dual flow thrust vector nozzles with post exit vanes
- Author: Carpenter, Thomas.
- Language: English
- Publisher: ➤ California Polytechnic State University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1992
- Publish Location: ➤ San Luis Obispo, Calif - Springfield, Va - [Washington, DC
“Design and evaluation of single and dual flow thrust vector nozzles with post exit vanes” Subjects and Themes:
- Subjects: Jet nozzles - Blades - Evaluation - Design and construction
Edition Identifiers:
- The Open Library ID: OL17679330M
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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36Experimental results of a deflected thrust V/STOL nozzle research program
By Paul L Burstadt
“Experimental results of a deflected thrust V/STOL nozzle research program” Metadata:
- Title: ➤ Experimental results of a deflected thrust V/STOL nozzle research program
- Author: Paul L Burstadt
- Language: English
- Number of Pages: Median: 24
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1983
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Experimental results of a deflected thrust V/STOL nozzle research program” Subjects and Themes:
- Subjects: Jet nozzles - Coriolis force
Edition Identifiers:
- The Open Library ID: OL14925782M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Effects of installation of F101 DFE exhaust nozzles on the afterbody-nozzle characteristics of the F-14 airplane
By David E Reubush
“Effects of installation of F101 DFE exhaust nozzles on the afterbody-nozzle characteristics of the F-14 airplane” Metadata:
- Title: ➤ Effects of installation of F101 DFE exhaust nozzles on the afterbody-nozzle characteristics of the F-14 airplane
- Author: David E Reubush
- Language: English
- Number of Pages: Median: 129
- Publisher: ➤ U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1982
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Effects of installation of F101 DFE exhaust nozzles on the afterbody-nozzle characteristics of the F-14 airplane” Subjects and Themes:
- Subjects: Jet nozzles - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL14925835M
Access and General Info:
- First Year Published: 1982
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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38A comparison of the noise produced by a small jet on a moving vehicle with that in a free jet
By Thomas D Norum
“A comparison of the noise produced by a small jet on a moving vehicle with that in a free jet” Metadata:
- Title: ➤ A comparison of the noise produced by a small jet on a moving vehicle with that in a free jet
- Author: Thomas D Norum
- Language: English
- Number of Pages: Median: 22
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office - for sale by the National Technical Information Service
- Publish Date: 1978
- Publish Location: [Washington] - Springfield, Va
“A comparison of the noise produced by a small jet on a moving vehicle with that in a free jet” Subjects and Themes:
- Subjects: Noise - Jet nozzles - Jet planes - Measurement
Edition Identifiers:
- The Open Library ID: OL14932205M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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39Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero
By Lawrence E. Putnam
“Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero” Metadata:
- Title: ➤ Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero
- Author: Lawrence E. Putnam
- Language: English
- Number of Pages: Median: 42
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1983
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Internal pressure distributions for a two-dimensional thrust-reversing nozzle operating at a free-stream mach number of zero” Subjects and Themes:
- Subjects: Jet nozzles - Jet planes - Thrust reversers
Edition Identifiers:
- The Open Library ID: OL14926282M
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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40Supersonic jets from bevelled rectangular nozzles
By Edward J. Rice
“Supersonic jets from bevelled rectangular nozzles” Metadata:
- Title: ➤ Supersonic jets from bevelled rectangular nozzles
- Author: Edward J. Rice
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Supersonic jets from bevelled rectangular nozzles” Subjects and Themes:
- Subjects: Jet nozzles
Edition Identifiers:
- The Open Library ID: OL17680108M
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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41An investigation into jet mixing similarity parameters proposed for solid-liquid mixtures
By Jeffrey Steven Johnson
“An investigation into jet mixing similarity parameters proposed for solid-liquid mixtures” Metadata:
- Title: ➤ An investigation into jet mixing similarity parameters proposed for solid-liquid mixtures
- Author: Jeffrey Steven Johnson
- Language: English
- Number of Pages: Median: 80
- Publish Date: 1994
“An investigation into jet mixing similarity parameters proposed for solid-liquid mixtures” Subjects and Themes:
- Subjects: Mixing - Jet nozzles - Slurry
Edition Identifiers:
- The Open Library ID: OL17004093M
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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42Mass transfer in an impinging jet
By Chu-jen Chia
“Mass transfer in an impinging jet” Metadata:
- Title: ➤ Mass transfer in an impinging jet
- Author: Chu-jen Chia
- Language: English
- Number of Pages: Median: 250
- Publish Date: 1972
- Publish Location: [Toronto]
“Mass transfer in an impinging jet” Subjects and Themes:
- Subjects: Transmission - Jet nozzles - Heat - Mass transfer
Edition Identifiers:
- The Open Library ID: OL19840328M
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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43Alternate nozzle ablative materials program
By N. A. Kimmel
“Alternate nozzle ablative materials program” Metadata:
- Title: ➤ Alternate nozzle ablative materials program
- Author: N. A. Kimmel
- Language: English
- Publisher: ➤ National Technical Information Service - The Laboratory
- Publish Date: 1984
- Publish Location: ➤ Pasadena, Calif - [Springfield, Va
“Alternate nozzle ablative materials program” Subjects and Themes:
- Subjects: Jet nozzles - Solid propellant rockets
Edition Identifiers:
- The Open Library ID: OL15394496M
Access and General Info:
- First Year Published: 1984
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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44Evaluation of water cooled supersonic temperature and pressure probes for application to 2000F̊ flows
By Nicholas T. Lagen
“Evaluation of water cooled supersonic temperature and pressure probes for application to 2000F̊ flows” Metadata:
- Title: ➤ Evaluation of water cooled supersonic temperature and pressure probes for application to 2000F̊ flows
- Author: Nicholas T. Lagen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Evaluation of water cooled supersonic temperature and pressure probes for application to 2000F̊ flows” Subjects and Themes:
- Subjects: Jet nozzles - Plumes (Fluid dynamics)
Edition Identifiers:
- The Open Library ID: OL15357377M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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45Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20
By Francis J. Capone
“Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20” Metadata:
- Title: ➤ Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20
- Author: Francis J. Capone
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Aeropropulsive characteristics of canted twin pitch-vectoring nozzles at Mach 0.20 to 1.20” Subjects and Themes:
- Subjects: Thrust - Jet nozzles - Testing - Airplanes - Motors
Edition Identifiers:
- The Open Library ID: OL15299686M
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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46Static internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capability
By Francis J. Capone
“Static internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capability” Metadata:
- Title: ➤ Static internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capability
- Author: Francis J. Capone
- 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: ➤ [Springfield, Va - [Washington, DC]
“Static internal performance of a single expansion ramp nozzle with multiaxis thrust vectoring capability” Subjects and Themes:
- Subjects: Thrust - Jet nozzles - Airplanes - Motors
Edition Identifiers:
- The Open Library ID: OL14696260M
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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47A nozzle internal performance prediction method
By John R. Carlson
“A nozzle internal performance prediction method” Metadata:
- Title: ➤ A nozzle internal performance prediction method
- Author: John R. Carlson
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“A nozzle internal performance prediction method” Subjects and Themes:
- Subjects: Jet nozzles - Aerodynamics
Edition Identifiers:
- The Open Library ID: OL14686565M
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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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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48Aeropropulsive 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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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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49Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle
By George T. Carson
“Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle” Metadata:
- Title: ➤ Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle
- Author: George T. Carson
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Effect of a trade between boattail angle and wedge size on the performance of a nonaxisymmetric wedge nozzle” Subjects and Themes:
- Subjects: Jet nozzles
Edition Identifiers:
- The Open Library ID: OL14663195M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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50Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring
By E. Ann Bare
“Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring” Metadata:
- Title: ➤ Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring
- Author: E. Ann Bare
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Static internal performance of a two-dimensional convergent-divergent nozzle with thrust vectoring” Subjects and Themes:
- Subjects: Jet nozzles
Edition Identifiers:
- The Open Library ID: OL14663227M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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