Explore: Thrust Vector Control
Discover books, insights, and more — all in one place.
Learn more about Thrust Vector Control with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “thrust-vector-control”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Optimal pitch thrust-vector angle and benefits for all flight regimes
By Glenn B. Gilyard
“Optimal pitch thrust-vector angle and benefits for all flight regimes” Metadata:
- Title: ➤ Optimal pitch thrust-vector angle and benefits for all flight regimes
- Author: Glenn B. Gilyard
- Language: English
- Number of Pages: Median: 22
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 2000
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Optimal pitch thrust-vector angle and benefits for all flight regimes” Subjects and Themes:
- Subjects: ➤ Airplanes - Angles (Geometry) - Automatic flight control - Control surfaces - Drag (Aerodynamics) - Flight testing - Handling characteristics - Lift (Aerodynamics) - Motors - Pitch (Inclination) - Thrust - Thrust vector control
Edition Identifiers:
- The Open Library ID: ➤ OL17704162M - OL20639635M - OL17596831M - OL18318816M - OL18302177M - OL18140962M
- Online Computer Library Center (OCLC) ID: 45009655
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Optimal pitch thrust-vector angle and benefits for all flight regimes at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
By Kenneth W. Iliff
“Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” Metadata:
- Title: ➤ Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring
- Author: Kenneth W. Iliff
- Language: English
- Number of Pages: Median: 65
- Publisher: ➤ National Technical Information Service, distributor - NASA, Dryden Flight Research Center - National Aeronautics and Space Administration, Dryden Flight Research Center - Available from National Technical Information Service
- Publish Date: 1997
- Publish Location: ➤ Edwards, Calif - Springfield, Va - [Springfield, Va
“Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring” Subjects and Themes:
- Subjects: ➤ Aircraft control - Airplanes - Angle of attack - Angle of attack (Aerodynamics) - Control surfaces - Control systems - Flight tests - Hornet (Jet fighter plane) - Longitudinal Stability of airplanes - Longitudinal stability - Maximum likelihood estimates - Parameter identification - Research vehicles - Thrust vector control - Unsteady aerodynamics - Yawing (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL19396278M - OL18134930M - OL17135417M - OL15548785M - OL17591853M
- Online Computer Library Center (OCLC) ID: 42758582
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.
Online Borrowing:
Online Marketplaces
Find Flight-determined subsonic longitudinal stability and control derivatives of the F-18 High Angle of Attack Research Vehicle (HARV) with thrust vectoring at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Static 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
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Electro-mechanical actuator
By Kenneth E. Schreiner
“Electro-mechanical actuator” Metadata:
- Title: Electro-mechanical actuator
- Author: Kenneth E. Schreiner
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Electro-mechanical actuator” Subjects and Themes:
- Subjects: ➤ Electromechanical devices - Mechanical drives - Actuators - Rocket engines - Induction motors - Aerospace systems - Space shuttle main engine - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL18121543M - OL15505203M - OL17593520M - OL17130668M
- Online Computer Library Center (OCLC) ID: 41297406
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:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Electro-mechanical actuator at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Effects 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
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Effects of internal yaw-vectoring devices on the static performance of a pitch-vectoring nonaxisymmetric convergent-divergent nozzle at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors
By Kenneth H. Goodrich
“A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors” Metadata:
- Title: ➤ A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors
- Author: Kenneth H. Goodrich
- Language: English
- Number of Pages: Median: 24
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors” Subjects and Themes:
- Subjects: Airplanes - Design and construction - Aerodynamic balance - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL18028695M - OL14662698M - OL15274282M - OL18931701M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A closed-form trim solution yielding minimum trim drag for airplanes with multiple longitudinal-control effectors at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7High-Alpha Research Vehicle (HARV) longitudinal controller
By Aaron J. Ostroff
“High-Alpha Research Vehicle (HARV) longitudinal controller” Metadata:
- Title: ➤ High-Alpha Research Vehicle (HARV) longitudinal controller
- Author: Aaron J. Ostroff
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“High-Alpha Research Vehicle (HARV) longitudinal controller” Subjects and Themes:
- Subjects: ➤ Aircraft control - Control systems design - Controllers - Design analysis - Feedback control - Feedforward control - Longitudinal control - Nonlinear systems - Research vehicles - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL16487211M - OL16982116M - OL15404315M - OL18076516M
- Online Computer Library Center (OCLC) ID: 32298600
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find High-Alpha Research Vehicle (HARV) longitudinal controller at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane
By David E. Reubush
“Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane” Metadata:
- Title: ➤ Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane
- Author: David E. Reubush
- Language: English
- Number of Pages: Median: 117
- Publisher: ➤ For sale by the National Technical Information Service] - Langley Research Center - National Aeronautics and Space Administration, Scientific and Technical Information Division
- Publish Date: 1987 - 1988
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va - [Springfield,Va - Hampton, Va
“Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Stability of airplanes - Drag - Yaw vanes - Thrust vector control - Blades
Edition Identifiers:
- The Open Library ID: OL17659289M - OL15274194M - OL17836819M - OL19251149M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Effects of the installation and operation of jet-exhaust yaw vanes on the longitudinal and lateral-directional characteristics of the F-14 airplane at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Flight testing the X-36--the test pilot's perspective
By Laurence A. Walker
“Flight testing the X-36--the test pilot's perspective” Metadata:
- Title: ➤ Flight testing the X-36--the test pilot's perspective
- Author: Laurence A. Walker
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor]
- Publish Date: 1997
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Flight testing the X-36--the test pilot's perspective” Subjects and Themes:
- Subjects: ➤ Aircraft performance - Angle of attack - Controllability - Flight tests - Fly by wire control - Remotely piloted Vehicles - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL17132642M - OL15548333M - OL18134794M - OL17583321M
- Online Computer Library Center (OCLC) ID: 41936959
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.
Online Borrowing:
Online Marketplaces
Find Flight testing the X-36--the test pilot's perspective at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Implicit 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
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Implicit time-marching solution of the Navier-Stokes equations for thrust reversing and thrust vectoring nozzle flows at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11The control system for the X-33 linear aerospike engine
By Jerry E. Jackson
“The control system for the X-33 linear aerospike engine” Metadata:
- Title: ➤ The control system for the X-33 linear aerospike engine
- Author: Jerry E. Jackson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1998
- Publish Location: ➤ [Washington, DC - Springfield, Va
“The control system for the X-33 linear aerospike engine” Subjects and Themes:
- Subjects: ➤ Control systems design - Thrust vector control - Throttling - Engine control - Single stage to orbit vehicles - X-33 reusable launch vehicle - Aerospike engines - Thrust control
Edition Identifiers:
- The Open Library ID: OL17701033M - OL17597325M
- Online Computer Library Center (OCLC) ID: 44273424
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find The control system for the X-33 linear aerospike engine at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊
By Scott C. Asbury
“Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊” Metadata:
- Title: ➤ Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊
- Author: Scott C. Asbury
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - Springfield, VA
“Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊” Subjects and Themes:
- Subjects: Nozzles - F-18 aircraft - Thrust vector control - Research vehicles
Edition Identifiers:
- The Open Library ID: OL18117381M - OL15494853M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70 ̊ at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
By Scott C. Asbury
“Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control” Metadata:
- Title: ➤ Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control
- Author: Scott C. Asbury
- 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
“Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control” Subjects and Themes:
- Subjects: Cavities - Exhaust nozzles - Hole geometry (Mechanics) - Porosity - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL17592116M - OL15559342M
- Online Computer Library Center (OCLC) ID: 43263577
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability
By David J. Wing
“Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability” Metadata:
- Title: ➤ Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability
- Author: David J. Wing
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1997
- Publish Location: ➤ Hampton, Va - [Springfield, Va - Washington, D.C
“Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability” Subjects and Themes:
- Subjects: ➤ Static models - Transonic wind tunnels - Thrust vector control - Nozzle flow - Internal flow - Convergent-divergent nozzles - Contours
Edition Identifiers:
- The Open Library ID: OL15504473M - OL21855558M
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.
Online Borrowing:
Online Marketplaces
Find Static investigation of a multiaxis thrust-vectoring nozzle with variable internal contouring ability at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft
By Martin J. Brenner
“Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft” Metadata:
- Title: ➤ Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft
- Author: Martin J. Brenner
- 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
“Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft” Subjects and Themes:
- Subjects: ➤ Aeroservoelasticity - Control theory - F-18 aircraft - Flight control - Structural stability - Thrust vector control - Vibration damping
Edition Identifiers:
- The Open Library ID: OL17593510M - OL15504490M
- Online Computer Library Center (OCLC) ID: 42721769
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:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Aeroservoelastic modeling and validation of a thrust-vectoring F/A-18 aircraft at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16An experimental/modeling study of jet attachment during counterflow thrust vectoring
By Paul J. Strykowski
“An experimental/modeling study of jet attachment during counterflow thrust vectoring” Metadata:
- Title: ➤ An experimental/modeling study of jet attachment during counterflow thrust vectoring
- Author: Paul J. Strykowski
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Springfield, Va
“An experimental/modeling study of jet attachment during counterflow thrust vectoring” Subjects and Themes:
- Subjects: Mathematical models - Counterflow - Aircraft engines - Thrust vector control - Jet flow
Edition Identifiers:
- The Open Library ID: OL17837321M - OL15505743M
- Online Computer Library Center (OCLC) ID: 40221323
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.
Online Borrowing:
Online Marketplaces
Find An experimental/modeling study of jet attachment during counterflow thrust vectoring at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17Integrated control using the SOFFT control structure
By Nesim Halyo
“Integrated control using the SOFFT control structure” Metadata:
- Title: ➤ Integrated control using the SOFFT control structure
- Author: Nesim Halyo
- Language: English
- Number of Pages: Median: 92
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, VA - Hampton, Va - [Springfield, Va
“Integrated control using the SOFFT control structure” Subjects and Themes:
- Subjects: ➤ F-15 aircraft - Control systems - Thrust vector control - Feedback - Propulsion - Airplanes - Feedforward control systems - Feedback control systems - Optimal control - Feedforward control
Edition Identifiers:
- The Open Library ID: OL19287933M - OL15504957M
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:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Integrated control using the SOFFT control structure at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
18Xenon ion propulsion for orbit transfer
By Vincent K. Rawlin
“Xenon ion propulsion for orbit transfer” Metadata:
- Title: ➤ Xenon ion propulsion for orbit transfer
- Author: Vincent K. Rawlin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Xenon ion propulsion for orbit transfer” Subjects and Themes:
- Subjects: ➤ Ion propulsion - Thrust vector control - Transfer orbits - Propulsion system performance - Propulsion system configurations - Power conditioning - Xenon - Stationkeeping
Edition Identifiers:
- The Open Library ID: OL15405961M
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:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Xenon ion propulsion for orbit transfer at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
19An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques
By William G. Schweikhard
“An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques” Metadata:
- Title: ➤ An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques
- Author: William G. Schweikhard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - University of Kansas - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Lawrence, Kan - Springfield, Va
“An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques” Subjects and Themes:
- Subjects: ➤ Jet engines - Test stands - Thrust vector control - Finite element method - Cross coupling - Nozzle thrust coefficients - Dynamic structural analysis
Edition Identifiers:
- The Open Library ID: OL18082691M - OL15416295M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
20HARV ANSER flight test data retrieval and processing procedures
By Jessie C. Yeager
“HARV ANSER flight test data retrieval and processing procedures” Metadata:
- Title: ➤ HARV ANSER flight test data retrieval and processing procedures
- Author: Jessie C. Yeager
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, Va
“HARV ANSER flight test data retrieval and processing procedures” Subjects and Themes:
- Subjects: ➤ Data retrieval - Thrust vector control - Data systems - Research vehicles - Data processing - Aircraft control
Edition Identifiers:
- The Open Library ID: OL17837095M - OL15498730M
- Online Computer Library Center (OCLC) ID: 39776157
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.
Online Borrowing:
Online Marketplaces
Find HARV ANSER flight test data retrieval and processing procedures at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
21A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane
By Frederick J. Lallman
“A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane” Metadata:
- Title: ➤ A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane
- Author: Frederick J. Lallman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: Springfield, VA - Hampton, Va
“A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane” Subjects and Themes:
- Subjects: ➤ Control stability - Thrust vector control - Feedback control - Angle of attack - Flight control - F-18 aircraft - Directional control - Fighter aircraft - Angular acceleration - Airplanes - Motors - Thrust - Control surfaces
Edition Identifiers:
- The Open Library ID: OL17598638M - OL15542778M
- Online Computer Library Center (OCLC) ID: 42814679
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A method for integrating thrust-vectoring and actuated forebody strakes with conventional aerodynamic controls on a high-performance fighter airplane at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
22A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring
By Steven A. Johnson
“A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring” Metadata:
- Title: ➤ A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring
- Author: Steven A. Johnson
- Language: English
- Number of Pages: Median: 18
- 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: ➤ Springfield, Va - [Washington, D.C.]
“A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring” Subjects and Themes:
- Subjects: ➤ Airplanes - Computer simulation - Dynamic models - F-18 aircraft - Motors - Real time operation - Real-time data processing - Scale models - Thrust - Thrust distribution - Thrust vector control - Turbofan engines
Edition Identifiers:
- The Open Library ID: OL16132236M
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:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23A control law design method facilitating control power, robustness, agility, and flying qualities tradeoffs, CRAFT
By Murphy, Patrick C.
“A control law design method facilitating control power, robustness, agility, and flying qualities tradeoffs, CRAFT” Metadata:
- Title: ➤ A control law design method facilitating control power, robustness, agility, and flying qualities tradeoffs, CRAFT
- Author: Murphy, Patrick C.
- 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
“A control law design method facilitating control power, robustness, agility, and flying qualities tradeoffs, CRAFT” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Control theory - Eigenvalues - Eigenvectors - Fighter aircraft - Flight control - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL15548825M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find A control law design method facilitating control power, robustness, agility, and flying qualities tradeoffs, CRAFT at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
24Electromechanical actuation for thrust vector control applications
By Mary Ellen Roth
“Electromechanical actuation for thrust vector control applications” Metadata:
- Title: ➤ Electromechanical actuation for thrust vector control applications
- Author: Mary Ellen Roth
- Language: English
- Publisher: ➤ NASA - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Electromechanical actuation for thrust vector control applications” Subjects and Themes:
- Subjects: ➤ Control systems - Thrust vector control - Advanced launch system (STS) - Actuators - Controllers - Algorithms - Induction motors - Technological innovations - Launch vehicles (Astronautics)
Edition Identifiers:
- The Open Library ID: OL16132908M
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:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Electromechanical actuation for thrust vector control applications at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
25Relative control effectiveness technique with application to airplane control coordination
By Frederick J. Lallman
“Relative control effectiveness technique with application to airplane control coordination” Metadata:
- Title: ➤ Relative control effectiveness technique with application to airplane control coordination
- Author: Frederick J. Lallman
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service,] - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Relative control effectiveness technique with application to airplane control coordination” Subjects and Themes:
- Subjects: ➤ Aircraft control - Aircraft stability - Airplanes - Control systems - Directional control - Lateral Stability of airplanes - Lateral control - Linear systems - Mathematical models - Mathematical optimization - Optimization - Stability of airplanes, Lateral - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL16115007M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Relative control effectiveness technique with application to airplane control coordination at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
26Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"
By Jing-Biau Tseng
“Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"” Metadata:
- Title: ➤ Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"
- Author: Jing-Biau Tseng
- Language: English
- Publisher: ➤ Flight Research Laboratory, University of Kansas Center for Research - National Aeronautics and Space Administration
- Publish Date: 1989
- Publish Location: ➤ [Washington, D.C - Lawrence, Kan
“Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring"” Subjects and Themes:
- Subjects: Aircraft stability - Attitude control - Thrust vector control - Nozzle thrust coefficients - Aircraft control
Edition Identifiers:
- The Open Library ID: OL16138003M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Semi-annual status report on NASA grant NAG 1-837, "Aerodynamics of thrust vectoring" at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
27Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 deg to 70 deg
By Scott C. Asbury
“Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 deg to 70 deg” Metadata:
- Title: ➤ Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 deg to 70 deg
- Author: Scott C. Asbury
- Number of Pages: Median: 173
- Publisher: Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va
“Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 deg to 70 deg” Subjects and Themes:
- Subjects: F-18 aircraft - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL19005431M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 deg to 70 deg at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
28Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70h̊
By Scott C. Asbury
“Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70h̊” Metadata:
- Title: ➤ Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70h̊
- Author: Scott C. Asbury
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1995
- Publish Location: Hampton, Va - Springfield, VA
“Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70h̊” Subjects and Themes:
- Subjects: Nozzles - F-18 aircraft - Thrust vector control - Research vehicles
Edition Identifiers:
- The Open Library ID: OL17122990M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Multiaxis thrust-vectoring characteristics of a model representative of the F-18 High-Alpha Research Vehicle at angles of attack from 0 ̊to 70h̊ at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
29Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
By George T. Carson
“Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability” Metadata:
- Title: ➤ Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability
- Author: George T. Carson
- 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, D.C
“Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability” Subjects and Themes:
- Subjects: ➤ Transonic wind tunnels - Axisymmetric flow - Thrust vector control - Wind tunnel tests - Nozzle design - Static tests - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL15405712M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Static internal performance of an axisymmetric nozzle with multiaxis thrust-vectoring capability at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
30Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle
By David J. Wing
“Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle” Metadata:
- Title: ➤ Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle
- 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 investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Thrust vector control - Coanda effect - Wind tunnel tests - Fluidics - Static tests - Flow visualization - Secondary flow - Two dimensional models - Two fluid models - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL15409385M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
31Static 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
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Static performance investigation of a skewed-throat multiaxis thrust-vectoring nozzle concept at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
32Static 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
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability
By Linda S. Bangert
“Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability” Metadata:
- Title: ➤ Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability
- Author: Linda S. Bangert
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: [Washington, D.C.]
“Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability” Subjects and Themes:
- Subjects: ➤ Jet planes - Thrust vector control - Wind tunnel tests - Testing - Static tests - Thrust reversal - Flow deflection - Deflectors - Thrust reversers
Edition Identifiers:
- The Open Library ID: OL16124006M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
34Evaluation of four advanced nozzle concepts for short takeoff and landing performance
By P. Frank Quinto
“Evaluation of four advanced nozzle concepts for short takeoff and landing performance” Metadata:
- Title: ➤ Evaluation of four advanced nozzle concepts for short takeoff and landing performance
- Author: P. Frank Quinto
- Number of Pages: Median: 95
- Publisher: Langley Research Center
- Publish Date: 1993
- Publish Location: Hampton, Va
“Evaluation of four advanced nozzle concepts for short takeoff and landing performance” Subjects and Themes:
- Subjects: Nozzles - Short takeoff aircraft - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL19916527M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Evaluation of four advanced nozzle concepts for short takeoff and landing performance at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
35Design of power electronics for TVC & EMA systems
By R. M. Nelms
“Design of power electronics for TVC & EMA systems” Metadata:
- Title: ➤ Design of power electronics for TVC & EMA systems
- Author: R. M. Nelms
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Design of power electronics for TVC & EMA systems” Subjects and Themes:
- Subjects: ➤ Electromechanical devices - Actuators - Electric motors - Power supply circuits - Inverters - Control equipment - Switching circuits - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL15409584M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Design of power electronics for TVC & EMA systems at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
36Static 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.
Online Borrowing:
Online Marketplaces
Find Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
37Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
By Mary L. Mason
“Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles” Metadata:
- Title: ➤ Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles
- Author: Mary L. Mason
- Language: English
- Number of Pages: Median: 216
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1985
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles” Subjects and Themes:
- Subjects: ➤ Thrust vector control - Motors - Wind tunnel tests - Testing - Airplanes - Static tests - Yawing (Aerodynamics) - Jet nozzles - Thrust - Yaw - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL16114743M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
38A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle
By Mary L. Mason
“A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle” Metadata:
- Title: ➤ A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle
- Author: Mary L. Mason
- Number of Pages: Median: 162
- Publisher: Langley Research Center
- Publish Date: 1992
- Publish Location: Hampton, Va
“A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle” Subjects and Themes:
- Subjects: Nozzles - Thrust vector control
Edition Identifiers:
- The Open Library ID: OL19244314M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find A static investigation of the thrust vectoring system of the F/A-18 high-alpha research vehicle at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
39Static 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.
Online Borrowing:
Online Marketplaces
Find Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
40Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers
By Robert S. Green
“Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers” Metadata:
- Title: ➤ Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers
- Author: Robert S. Green
- Number of Pages: Median: 40
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers” Subjects and Themes:
- Subjects: Nozzles - Thrust vector control - Thrust reversal
Edition Identifiers:
- The Open Library ID: OL18998644M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
41Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle
By W. Thomas Bundick
“Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle” Metadata:
- Title: ➤ Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle
- Author: W. Thomas Bundick
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: [Springfield, Va - Hampton, Va
“Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle” Subjects and Themes:
- Subjects: ➤ Flight control - Control systems design - Thrust vector control - Flight simulation - Vanes - Flight tests
Edition Identifiers:
- The Open Library ID: OL17834495M
- Online Computer Library Center (OCLC) ID: 39535884
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:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Design of a mixer for the thrust-vectoring system on the high-alpha research vehicle at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
42Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application
By Jagdish S. Sokhey
“Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application” Metadata:
- Title: ➤ Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application
- Author: Jagdish S. Sokhey
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application” Subjects and Themes:
- Subjects: ➤ Viscous flow - Powered lift aircraft - Vertical landing - Thrust vector control - Exhaust nozzles - Nozzle flow - Analysis (Mathematics)
Edition Identifiers:
- The Open Library ID: OL15539894M
- Online Computer Library Center (OCLC) ID: 40763709
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.
Online Borrowing:
Online Marketplaces
Find Development of a telescoping vaned exhaust nozzle for the ASTOVL LiftFan application at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.