Explore: Canard Configurations
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Source: The Open Library
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11999 NASA High-Speed Research Program Aerodynamic Performance Workshop
By NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)
“1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” Metadata:
- Title: ➤ 1999 NASA High-Speed Research Program Aerodynamic Performance Workshop
- Author: ➤ NASA High-Speed Research Program Aerodynamic Performance Workshop (1999 Anaheim, Calif.)
- 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
“1999 NASA High-Speed Research Program Aerodynamic Performance Workshop” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic configurations - Aerodynamic stability - Aerodynamics - Aerodynamics, Supersonic - Aeronautics, Commercial - Aircraft design - Airplanes - Body-wing configurations - Canard configurations - Civil aviation - Commercial Aeronautics - Computational fluid dynamics - Congresses - Design and construction - Engine airframe integration - High-speed aeronautics - Optimization - Performance prediction - Research - Supersonic Aerodynamics - Supersonic transports - Wind tunnel tests - Wing nacelle configurations
Edition Identifiers:
- The Open Library ID: OL18140721M - OL18296463M - OL22405471M - OL15573231M - OL17594870M
- Online Computer Library Center (OCLC) ID: 44596209
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
By Long P. Yip
“Wind-tunnel investigation of a full-scale canard-configured general aviation airplane” Metadata:
- Title: ➤ Wind-tunnel investigation of a full-scale canard-configured general aviation airplane
- Author: Long P. Yip
- Language: English
- Publisher: ➤ National; Aeronautics and Space Administration Scientific and Technical Information Branch - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: [s.l.] - [Washington, D.C.]
“Wind-tunnel investigation of a full-scale canard-configured general aviation airplane” Subjects and Themes:
- Subjects: ➤ Control stability - Canard configurations - Control surfaces - Wind tunnel tests - General aviation aircraft - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL13839737M - OL16116833M - OL18218708M
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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3Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration
By Dale R. Satran
“Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration” Metadata:
- Title: ➤ Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration
- Author: Dale R. Satran
- Language: English
- Number of Pages: Median: 56
- Publisher: ➤ National Aewronautics and Space Administration, Scientific and Technical Information Branch - Langley Research Center - For sale by National Technical Information Service]
- Publish Date: 1986
- Publish Location: ➤ [Washington, DC] - Hampton, Va - [Springfield, Va
“Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration” Subjects and Themes:
- Subjects: ➤ Airplanes - Canard Wings - Canard configurations - General aviation aircraft - Stability - Stability of airplanes - Wings, Canard
Edition Identifiers:
- The Open Library ID: OL15273061M - OL20984795M - OL16371092M - OL18028127M
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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4Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system
By Daniel W. Banks
“Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system” Metadata:
- Title: ➤ Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system
- Author: Daniel W. Banks
- Language: English
- Number of Pages: Median: 112
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor] - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1987
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“Low-speed aerodynamic characteristics of a wing-canard configuration with underwing spanwise blowing on the trailing-edge flap system” Subjects and Themes:
- Subjects: Trailing edge flaps - Canard configurations - Spanwise blowing - Low speed - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL20986801M - OL18080186M - OL17683879M - OL17115110M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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5HiMAT flight program
By Dwain A. Deets
“HiMAT flight program” Metadata:
- Title: HiMAT flight program
- Author: Dwain A. Deets
- Language: English
- Number of Pages: Median: 28
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - Ames Research Center - For sale by the National Technical Information Service]
- Publish Date: 1986 - 1987
- Publish Location: ➤ [Washington, DC] - Edwards, Calif - [Springfield, Va
“HiMAT flight program” Subjects and Themes:
- Subjects: Canard configurations - Composite structures - Remotely piloted Vehicles - Research aircraft - Scale effect
Edition Identifiers:
- The Open Library ID: OL20899272M - OL15288187M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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6Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport
By Christopher A. Lee
“Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport” Metadata:
- Title: ➤ Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport
- Author: Christopher A. Lee
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ San Jose, CA - Springfield, Va - [Washington, DC
“Design and testing of low sonic boom configurations and an oblique all-wing supersonic transport” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Canard configurations - Design analysis - Performance tests - Sonic booms - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL15413726M - OL17791642M
- Online Computer Library Center (OCLC) ID: 33431926
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
By Matthew Robert Whiting
“Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail” Metadata:
- Title: ➤ Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail
- Author: Matthew Robert Whiting
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail” Subjects and Themes:
- Subjects: ➤ X-31 - Canard configurations - Directional control - Wind tunnel tests - Drop tests - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15423353M - OL17796404M
- Online Computer Library Center (OCLC) ID: 35270882
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.
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8Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)
By Joanne L. Walsh
“Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)” Metadata:
- Title: ➤ Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)
- Author: Joanne L. Walsh
- Language: English
- Number of Pages: Median: 113
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2005
- Publish Location: Hampton, Va
“Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP)” Subjects and Themes:
- Subjects: ➤ Body-wing configurations - Canard configurations - Aeroelasticity - Sandwich structures - Longitudinal control - Design analysis - Composite materials
Edition Identifiers:
- The Open Library ID: OL43894466M
- Online Computer Library Center (OCLC) ID: 781856606
Access and General Info:
- First Year Published: 2005
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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9Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization
By Harry W. Carlson
“Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization” Metadata:
- Title: ➤ Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization
- Author: Harry W. Carlson
- Number of Pages: Median: 122
- Publisher: Langley Research center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Validation of a computer code for analysis of subsonic aerodynamic performance of wings with flaps in combination with a canard or horizontal tail and an application to optimization” Subjects and Themes:
- Subjects: Flaps - Canard configurations
Edition Identifiers:
- The Open Library ID: OL19380340M
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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10A computer module used to calculate the horizontal control surface size of a conceputal aircraft design
By Doral R. Sandlin
“A computer module used to calculate the horizontal control surface size of a conceputal aircraft design” Metadata:
- Title: ➤ A computer module used to calculate the horizontal control surface size of a conceputal aircraft design
- Author: Doral R. Sandlin
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - California Polytechnic State University, Aeronautical Engineering Dept. - National Aeronautics and Space Administration
- Publish Date: 1990
- Publish Location: ➤ San Luis Obispo, Calif - [Washington, D.C.] - [Springfield, Va
“A computer module used to calculate the horizontal control surface size of a conceputal aircraft design” Subjects and Themes:
- Subjects: ➤ Mathematical models - Computer aided design - Canard configurations - Aircraft design.. - Control surfaces - Computer programs - Design analysis
Edition Identifiers:
- The Open Library ID: OL16138013M
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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11Parametric study of a canard-configured transport using conceptual design optimization
By P. Douglas Arbuckle
“Parametric study of a canard-configured transport using conceptual design optimization” Metadata:
- Title: ➤ Parametric study of a canard-configured transport using conceptual design optimization
- Author: P. Douglas Arbuckle
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: [Washington, D.C.]
“Parametric study of a canard-configured transport using conceptual design optimization” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aircraft design - Airplanes - Canard Wings - Canard configurations - Design and construction - Jet transports - Mathematical optimization - Tandem wing aircraft - Wings, Canard
Edition Identifiers:
- The Open Library ID: OL16114856M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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12Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
By Ira J. Walker
“Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Metadata:
- Title: ➤ Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0
- Author: Ira J. Walker
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1993
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0” Subjects and Themes:
- Subjects: ➤ Stabilizers (Fluid dynamics) - Canard configurations - Hypersonics - Aerodynamic characteristics - Delta wings - Wind tunnel tests - Research vehicles - Mach number - Hypersonic vehicles - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15403234M
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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13Numerical study of steady and unsteady canard-wing-body aerodynamics
By Eugene L. Tu
“Numerical study of steady and unsteady canard-wing-body aerodynamics” Metadata:
- Title: ➤ Numerical study of steady and unsteady canard-wing-body aerodynamics
- Author: Eugene L. Tu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Numerical study of steady and unsteady canard-wing-body aerodynamics” Subjects and Themes:
- Subjects: ➤ Navier-Stokes equation - Unsteady aerodynamics - Canard configurations - Aircraft configurations - Aerodynamic characteristics - Control surfaces - Aerodynamic configurations - Flow distribution - Wings
Edition Identifiers:
- The Open Library ID: OL15498139M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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14Space shuttle orbiter trimmed center-of-gravity extension study
By William I. Scallion
“Space shuttle orbiter trimmed center-of-gravity extension study” Metadata:
- Title: ➤ Space shuttle orbiter trimmed center-of-gravity extension study
- Author: William I. Scallion
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1985
- Publish Location: Washington, D.C
“Space shuttle orbiter trimmed center-of-gravity extension study” Subjects and Themes:
- Subjects: Space shuttle orbiters - Center of gravity - Canard configurations - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL16116808M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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15Visualisation in water of vortex flow over sharp-edged canard configurations
By D. H. Thompson
“Visualisation in water of vortex flow over sharp-edged canard configurations” Metadata:
- Title: ➤ Visualisation in water of vortex flow over sharp-edged canard configurations
- Author: D. H. Thompson
- Number of Pages: Median: 40
- Publisher: ➤ Australia, Dept. of Defence, Aeronautical Research Laboratory
- Publish Date: 1992
- Publish Location: Melbourne, Victoria
“Visualisation in water of vortex flow over sharp-edged canard configurations” Subjects and Themes:
- Subjects: Canard configurations - Water tunnel tests - Flow visualization - Vortices
Edition Identifiers:
- The Open Library ID: OL19245372M
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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16Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails
By Jerry M. Allen
“Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails” Metadata:
- Title: ➤ Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails
- Author: Jerry M. Allen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, Va
“Experimental study at low supersonic speeds of a missile concept having opposing wraparound tails” Subjects and Themes:
- Subjects: ➤ Canard configurations - Missile configurations - Missile control - Rolling moments - Supersonic speed - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15408442M
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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17A theoretical study of the aerodynamic characteristics of low-speed multi-wing aircraft
By Bernard Gagnon
“A theoretical study of the aerodynamic characteristics of low-speed multi-wing aircraft” Metadata:
- Title: ➤ A theoretical study of the aerodynamic characteristics of low-speed multi-wing aircraft
- Author: Bernard Gagnon
- Publisher: ➤ Dept. of Aerospace Science and Engineering
- Publish Date: 1983
- Publish Location: [Downsview, Ont.]
“A theoretical study of the aerodynamic characteristics of low-speed multi-wing aircraft” Subjects and Themes:
- Subjects: Aerodynamic characteristics - Canard configurations
Edition Identifiers:
- The Open Library ID: OL22344547M
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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