Explore: Tail Assemblies
Discover books, insights, and more — all in one place.
Learn more about Tail Assemblies with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “tail-assemblies”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Numerical simulation of the SOFIA flowfield
By Stephen P. Klotz
“Numerical simulation of the SOFIA flowfield” Metadata:
- Title: ➤ Numerical simulation of the SOFIA flowfield
- Author: Stephen P. Klotz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - San Jose, CA
“Numerical simulation of the SOFIA flowfield” Subjects and Themes:
- Subjects: ➤ Active control - Aerodynamic stalling - Airfoils - Boeing 747 aircraft - Boundary layer control - Cavities - Flow distribution - Leading edges - SOFIA (Airborne observatory) - Separated flow - Sound pressure - Tail assemblies - Telescopes - Unsteady flow - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17788523M - OL17791647M - OL18081185M - OL18078541M - OL17683431M
- Online Computer Library Center (OCLC) ID: 33433883 - 32647393
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 Numerical simulation of the SOFIA flowfield at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
By Charles Michael Fremaux
“Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Metadata:
- Title: ➤ Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails
- Author: Charles Michael Fremaux
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - For sale by the National Technical Information Service
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, Va
“Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails” Subjects and Themes:
- Subjects: Reynolds number - Wind tunnel tests - Research vehicles - Tail assemblies - Spin tests
Edition Identifiers:
- The Open Library ID: OL17834292M - OL18114842M - OL17123433M - OL15487251M
- Online Computer Library Center (OCLC) ID: 39098301
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 Spin-tunnel investigation of a 1/28-scale model of the NASA F-18 High Alpha Research Vehicle (HARV) with and without vertical tails at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
By Scott P. Fears
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Metadata:
- Title: ➤ Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊
- Author: Scott P. Fears
- Language: English
- Number of Pages: Median: 145
- Publisher: ➤ National Aeronautics and Space Administration - Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Hampton, Va - [Washington, DC - Springfield, Va
“Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊” Subjects and Themes:
- Subjects: ➤ Trailing edge flaps - Aspect ratio - Flight stability tests - Stabilizers (Fluid dynamics) - Wind tunnel tests - Wing profiles - Aerodynamic stability - Angle of attack - Stability - Flight control - Low speed - Planforms - Arrow wings - Tail assemblies - Leading edge flaps
Edition Identifiers:
- The Open Library ID: OL19003591M - OL15416719M - OL18082907M - OL17032232M
- Online Computer Library Center (OCLC) ID: 34127880
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 Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50 ̊ at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds
By William P. Henderson
“Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds” Metadata:
- Title: ➤ Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds
- Author: William P. Henderson
- Language: English
- 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, DC] - Hampton, Va - [Springfield, Va
“Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds” Subjects and Themes:
- Subjects: Aerodynamics, Transonic - Nozzles - Tail assemblies - Transonic Aerodynamics - Transonic speed
Edition Identifiers:
- The Open Library ID: OL19250322M - OL14664598M
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 Effect of empennage arrangement on single engine nozzle/afterbody static pressures at transonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
By Stacey J. Cotton
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Metadata:
- Title: ➤ Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model
- Author: Stacey J. Cotton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Buffeting - Flight tests - Flow visualization - Liquid-vapor interfaces - Scale models - Sideslip - Stabilizers (Fluid dynamics) - Tail assemblies - Vortices - Water tunnel tests - X-29 aircraft
Edition Identifiers:
- The Open Library ID: OL17001977M - OL17682958M - OL18076527M
- Online Computer Library Center (OCLC) ID: 32298726
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 Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Flow-field survey of an empennage wake interacting with a pusher propeller
By W. Clifton Horne
“Flow-field survey of an empennage wake interacting with a pusher propeller” Metadata:
- Title: ➤ Flow-field survey of an empennage wake interacting with a pusher propeller
- Author: W. Clifton Horne
- Language: English
- Number of Pages: Median: 51
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
- Publish Date: 1988
- Publish Location: ➤ Moffett Field, Calif - Springfield, Va
“Flow-field survey of an empennage wake interacting with a pusher propeller” Subjects and Themes:
- Subjects: ➤ Aerial Propellers - Flow distribution - Interactions - Noise - Propellers - Propellers, Aerial - Pushing - Tail assemblies - Wakes
Edition Identifiers:
- The Open Library ID: OL18078062M - OL15407160M - OL17114421M
Access and General Info:
- First Year Published: 1988
- 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 Flow-field survey of an empennage wake interacting with a pusher propeller at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
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.
Online Borrowing:
Online Marketplaces
Find Differential canard deflection for generation of yawing moment on the X-31 with and without the vertical tail at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes
By James S. Bowman
“Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes” Metadata:
- Title: ➤ Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes
- Author: James S. Bowman
- Language: English
- Number of Pages: Median: 82
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - For sale by the National Technical Information Service]
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - [Washington, D.C.]
“Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes” Subjects and Themes:
- Subjects: ➤ Statistics - Measurement - Fuselages - Spin (Aerodynamics) - Pressure measurement - Aircraft models - Airplanes - Pressure - Spin tests - Fuselage - Tail assemblies - Aerodynamic load
Edition Identifiers:
- The Open Library ID: OL16137794M
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 Measurements of pressures on the tail and aft fuselage of an airplane model during rotary motions at spin attitudes at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles
By Mark C. Frassinelli
“Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles” Metadata:
- Title: ➤ Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles
- Author: Mark C. Frassinelli
- Number of Pages: Median: 56
- Publisher: Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va
“Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles” Subjects and Themes:
- Subjects: F-15 aircraft - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL21333297M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Effect of tail size reductions on longitudinal aerodynamic characteristics of a three-surface F-15 model with nonaxisymmetric nozzles at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Numerical simulation of the SOFIA flow field
By Stephen P. Klotz
“Numerical simulation of the SOFIA flow field” Metadata:
- Title: ➤ Numerical simulation of the SOFIA flow field
- Author: Stephen P. Klotz
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - MCAT Institute - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - San Jose, CA
“Numerical simulation of the SOFIA flow field” Subjects and Themes:
- Subjects: ➤ Boeing 747 aircraft - Cavities - Flow distribution - SOFIA (Airborne observatory) - Sound pressure - Tail assemblies - Telescopes
Edition Identifiers:
- The Open Library ID: OL17683980M
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 Numerical simulation of the SOFIA flow field at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Tailless aircraft performance improvements
By Irving Louis Ashkenas
“Tailless aircraft performance improvements” Metadata:
- Title: ➤ Tailless aircraft performance improvements
- Author: Irving Louis Ashkenas
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va - [Springfield, Va
“Tailless aircraft performance improvements” Subjects and Themes:
- Subjects: ➤ Aircraft configurations - Aircraft control - Aircraft performance - Remotely piloted Vehicles - Static stability - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15407752M
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 Tailless aircraft performance improvements at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet
By Robert W. Moses
“A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet” Metadata:
- Title: ➤ A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet
- Author: Robert W. Moses
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va - [Springfield, Va
“A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet” Subjects and Themes:
- Subjects: ➤ Bending moments - Pressure distribution - Pressure measurement - Wind tunnel tests - Full scale tests - Angle of attack - Buffeting - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15503560M
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 A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Some buffet response characteristics of a twin-vertical-tail configuration
By Stanley R. Cole
“Some buffet response characteristics of a twin-vertical-tail configuration” Metadata:
- Title: ➤ Some buffet response characteristics of a twin-vertical-tail configuration
- Author: Stanley R. Cole
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“Some buffet response characteristics of a twin-vertical-tail configuration” Subjects and Themes:
- Subjects: ➤ Stabilizers (Fluid dynamics) - Stiffness - Buffeting - Wind tunnel tests - Aircraft configurations - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15405530M
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 Some buffet response characteristics of a twin-vertical-tail configuration at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Experimental 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
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 Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
15Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters
By Cynthia A. Crowell
“Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters” Metadata:
- Title: ➤ Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters
- Author: Cynthia A. Crowell
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1990
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters” Subjects and Themes:
- Subjects: ➤ Wind direction - Strakes - Helicopter control - Cross flow - Helicopter performance - Wind tunnel tests - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL15405518M
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 Aerodynamic effect of strakes on two-dimensional tail boom models of OH-58A and OH-58D helicopters at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
16Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane
By H. Paul Stough
“Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane” Metadata:
- Title: ➤ Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane
- Author: H. Paul Stough
- Number of Pages: Median: 122
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane” Subjects and Themes:
- Subjects: Stalling - Spin tests - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL18998086M
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 Flight investigation of the effect of tail configuration on stall, spin, and recovery characteristics of a low-wing general aviation research airplane at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
17Vertical-tail loads in the rolling pull-out manoeuvre
By J. G. Rolland Collette
“Vertical-tail loads in the rolling pull-out manoeuvre” Metadata:
- Title: ➤ Vertical-tail loads in the rolling pull-out manoeuvre
- Author: J. G. Rolland Collette
- Number of Pages: Median: 22
- Publisher: [Institute of Aerophysics]
- Publish Date: 1952
- Publish Location: [Downsview, Ont.]
“Vertical-tail loads in the rolling pull-out manoeuvre” Subjects and Themes:
- Subjects: Rolling pull-out manoeuvre - Tail assemblies
Edition Identifiers:
- The Open Library ID: OL18999644M
Access and General Info:
- First Year Published: 1952
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Vertical-tail loads in the rolling pull-out manoeuvre at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.