Explore: Trailing Edges
Discover books, insights, and more — all in one place.
Learn more about Trailing Edges with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “trailing-edges”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Two-dimensional converging-diverging rippled nozzles at transonic speeds
By John R. Carlson
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Metadata:
- Title: ➤ Two-dimensional converging-diverging rippled nozzles at transonic speeds
- Author: John R. Carlson
- Language: English
- Number of Pages: Median: 105
- Publisher: ➤ Langley Research Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1994
- Publish Location: ➤ Hampton - Hampton, Va - [Springfield, Va
“Two-dimensional converging-diverging rippled nozzles at transonic speeds” Subjects and Themes:
- Subjects: ➤ Convergent-divergent nozzles - Discharge coefficient - Drag - Nozzle flow - Nozzle geometry - Nozzles - Ripples - Thrust - Trailing edges - Transonic speed - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: ➤ OL19752932M - OL16487219M - OL15403665M - OL16982124M - OL19753709M - OL18076297M
- Online Computer Library Center (OCLC) ID: 32220800
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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 Two-dimensional converging-diverging rippled nozzles at transonic speeds at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Assessment of dual-point drag reduction for an executive-jet modified airfoil section
By Dennis O. Allison
“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Metadata:
- Title: ➤ Assessment of dual-point drag reduction for an executive-jet modified airfoil section
- Author: Dennis O. Allison
- Language: English
- Number of Pages: Median: 114
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from National Technical Information Center - National Technical Information Service, distributor - National Aeronautics and Space Administration, Langly Research Center
- Publish Date: 1996
- Publish Location: ➤ Hampton, Virginia - Springfield, VA - Hampton, Va - [Springfield, Va
“Assessment of dual-point drag reduction for an executive-jet modified airfoil section” Subjects and Themes:
- Subjects: ➤ Drag reduction - Reynolds number - Boundary layer transition - Angle of attack - Pitching moments - Transonic wind tunnels - Airfoil profiles - Force distribution - Trailing edges - Aerodynamic characteristics - Aerodynamics - Aerofoils
Edition Identifiers:
- The Open Library ID: OL19049550M - OL18121248M - OL17126940M - OL17581020M - OL15504416M
- Online Computer Library Center (OCLC) ID: 40386607
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 Assessment of dual-point drag reduction for an executive-jet modified airfoil section at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3High-lift systems on commercial subsonic airliners
By Peter K. C. Rudolph
“High-lift systems on commercial subsonic airliners” Metadata:
- Title: ➤ High-lift systems on commercial subsonic airliners
- Author: Peter K. C. Rudolph
- Language: English
- Number of Pages: Median: 155
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“High-lift systems on commercial subsonic airliners” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Aeronautics, Commercial - Airplanes - Attitude (Inclination) - Commercial Aeronautics - Commercial aircraft - Cost analysis - Design analysis - Design and construction - Leading edge flaps - Leading edges - Lift (Aerodynamics) - Lift devices - Trailing edge flaps - Trailing edges - Wing camber - Wing loading - Wing slots
Edition Identifiers:
- The Open Library ID: OL15504955M - OL17576368M - OL18121439M - OL17125763M - OL19287956M
- Online Computer Library Center (OCLC) ID: 39916172
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 High-lift systems on commercial subsonic airliners at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Flow characteristics about a trailing edge
By Dwayne S. Smith
“Flow characteristics about a trailing edge” Metadata:
- Title: ➤ Flow characteristics about a trailing edge
- Author: Dwayne S. Smith
- Number of Pages: Median: 53
- Publisher: ➤ Institute for Aerospace Studies - Institute for Aerospace Studies, University of Toronto
- Publish Date: 1988 - 1989
- Publish Location: [Downsview, Ont.]
“Flow characteristics about a trailing edge” Subjects and Themes:
- Subjects: Flow characteristics - Trailing edged - Trailing edges - Wakes
Edition Identifiers:
- The Open Library ID: OL18926508M - OL21041110M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Flow characteristics about a trailing edge at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
5Predicting modes of the unsteady vorticity field near the trailing edge of a blade
By William J. Devenport
“Predicting modes of the unsteady vorticity field near the trailing edge of a blade” Metadata:
- Title: ➤ Predicting modes of the unsteady vorticity field near the trailing edge of a blade
- Author: William J. Devenport
- Language: English
- Publisher: ➤ National Technical Information Service [distributor - Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2003
- Publish Location: ➤ Hanover, MD - Springfield, VA - [Cleveland, Ohio]
“Predicting modes of the unsteady vorticity field near the trailing edge of a blade” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Turbulent boundary layer - Vorticity - Turbulence models - Flow distribution - Noise prediction (Aircraft) - Trailing edges - Aerodynamic noise
Edition Identifiers:
- The Open Library ID: OL17633148M - OL17722592M
- Online Computer Library Center (OCLC) ID: 56828333
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
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 Predicting modes of the unsteady vorticity field near the trailing edge of a blade at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Development of direct-inverse 3-D method for applied aerodynamic design and analysis
By Leland A. Carlson
“Development of direct-inverse 3-D method for applied aerodynamic design and analysis” Metadata:
- Title: ➤ Development of direct-inverse 3-D method for applied aerodynamic design and analysis
- Author: Leland A. Carlson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Texas Engineering Experiment Station, Aerospace Engineering Department, Texas A&M University
- Publish Date: 1987
- Publish Location: ➤ College Station, Tex - Springfield, Va - [Washington, DC
“Development of direct-inverse 3-D method for applied aerodynamic design and analysis” Subjects and Themes:
- Subjects: ➤ Flow equations - Body-wing configurations - Aerodynamics - Coordinates - Design analysis - Transonic flight - Trailing edges - Computer aided design - Aircraft design - Potential flow - Wings
Edition Identifiers:
- The Open Library ID: OL15412083M - OL18080134M
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 Development of direct-inverse 3-D method for applied aerodynamic design and analysis at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Heat transfer in a complex trailing edge passage for a high pressure turbine blade
By D. L. Rigby
“Heat transfer in a complex trailing edge passage for a high pressure turbine blade” Metadata:
- Title: ➤ Heat transfer in a complex trailing edge passage for a high pressure turbine blade
- Author: D. L. Rigby
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2002
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Heat transfer in a complex trailing edge passage for a high pressure turbine blade” Subjects and Themes:
- Subjects: ➤ High pressure - Trailing edges - Computerized simulation - Heat transfer coefficients - Three dimensional flow - Turbine blades
Edition Identifiers:
- The Open Library ID: OL16111312M - OL17621431M
- Online Computer Library Center (OCLC) ID: 56040841
Access and General Info:
- First Year Published: 2002
- 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 Heat transfer in a complex trailing edge passage for a high pressure turbine blade at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation
By Atlee M. Cunningham
“A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation” Metadata:
- Title: ➤ A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation
- Author: Atlee M. Cunningham
- Number of Pages: Median: 79
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation” Subjects and Themes:
- Subjects: Reynolds number - Transonic flow - Trailing edges - Mach number
Edition Identifiers:
- The Open Library ID: OL22344657M
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 A study of the effects of Reynolds number and Mach number on constant pressure coefficient jump for shock-induced trailing-edge separation at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Trailing edge flow conditions as a factor in airfoil design
By A. I. Ormsbee
“Trailing edge flow conditions as a factor in airfoil design” Metadata:
- Title: ➤ Trailing edge flow conditions as a factor in airfoil design
- Author: A. I. Ormsbee
- Language: English
- Publisher: ➤ Aeronautical and Astronautical Engineering Dept., University of Illinois - National Aeronautics and Space Administration
- Publish Date: 1984
- Publish Location: Urbana, Ill - [Washington, DC
“Trailing edge flow conditions as a factor in airfoil design” Subjects and Themes:
- Subjects: ➤ Pressure gradients - Trailing edges (Aerodynamics) - Design and construction - Trailing edges - Airfoils - Aircraft design - Potential flow - Aerofoils
Edition Identifiers:
- The Open Library ID: OL16153716M
Access and General Info:
- First Year Published: 1984
- 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 Trailing edge flow conditions as a factor in airfoil design at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10NACA 0015 wing pressure and trailing vortex measurements
By Kenneth W. McAlister
“NACA 0015 wing pressure and trailing vortex measurements” Metadata:
- Title: ➤ NACA 0015 wing pressure and trailing vortex measurements
- Author: Kenneth W. McAlister
- Language: English
- Publisher: ➤ National Technical Information Service , distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“NACA 0015 wing pressure and trailing vortex measurements” Subjects and Themes:
- Subjects: ➤ Vortices - Pressure measurement - Wing tips - Velocity measurement - Trailing edges - Low speed - Semispan models - Wings
Edition Identifiers:
- The Open Library ID: OL17725370M
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 NACA 0015 wing pressure and trailing vortex measurements at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
By Dennis O. Allison
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Metadata:
- Title: ➤ Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane
- Author: Dennis O. Allison
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service (NTIS) [distributor
- Publish Date: 1995
- Publish Location: Springfield, VA - Hampton, Va
“Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane” Subjects and Themes:
- Subjects: ➤ Pressure distribution - Wind tunnel tests - Aircraft models - Subsonic speed - Transonic speed - Maneuverability - Trailing edges - Airfoils - Wing-fuselage stores - Leading edges
Edition Identifiers:
- The Open Library ID: OL15413576M
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 Airfoil modification effects on subsonic and transonic pressure distributions and performance for the EA-6B airplane at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
12Attached and separated trailing edge flow measurements with a triple-split hot-film probe
By Michael Donald Doiron
“Attached and separated trailing edge flow measurements with a triple-split hot-film probe” Metadata:
- Title: ➤ Attached and separated trailing edge flow measurements with a triple-split hot-film probe
- Author: Michael Donald Doiron
- Number of Pages: Median: 111
- Publisher: ➤ University of Toronto, Graduate Department of Aerospace Science and Engineering
- Publish Date: 1992
- Publish Location: [Toronto, Ont.]
“Attached and separated trailing edge flow measurements with a triple-split hot-film probe” Subjects and Themes:
- Subjects: Hot-film anemometers - Trailing edges - Separated flow
Edition Identifiers:
- The Open Library ID: OL19246488M
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 Attached and separated trailing edge flow measurements with a triple-split hot-film probe at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
13Optimum transonic airfoils based on the Euler equations
By Angelo Iollo
“Optimum transonic airfoils based on the Euler equations” Metadata:
- Title: ➤ Optimum transonic airfoils based on the Euler equations
- Author: Angelo Iollo
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Optimum transonic airfoils based on the Euler equations” Subjects and Themes:
- Subjects: Euler equations of motion - Transonic flight - Trailing edges - Airfoils - Transonic flow
Edition Identifiers:
- The Open Library ID: OL15505106M
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 Optimum transonic airfoils based on the Euler equations at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
14Asymptotic behavior of a flat plate wake
By James H. Weygandt
“Asymptotic behavior of a flat plate wake” Metadata:
- Title: ➤ Asymptotic behavior of a flat plate wake
- Author: James H. Weygandt
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1989
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Asymptotic behavior of a flat plate wake” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Flat plates - Fluid dynamics - Far fields - Wakes - Trailing edges
Edition Identifiers:
- The Open Library ID: OL15409352M
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 Asymptotic behavior of a flat plate wake at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Trailing edge
exerted by the sharp trailing edge of an aerofoil on the circulation.” Other sharp-edged surfaces that are attached to the trailing edges of wings or control
Flap (aeronautics)
aircraft wing at a given weight. Flaps are usually mounted on the wing trailing edges of a fixed-wing aircraft. Flaps are used to reduce the take-off distance
Chord (aeronautics)
edge and trailing edge of an aerofoil cross section parallel to the direction of the airflow. The chord length is the distance between the trailing edge
Chengdu J-36
one leading-edge extension (LRX) and five trailing edge control surfaces on each wing (including two split flap rudders at outboard wing edges), multiple
Gurney flap
The Gurney flap (or wickerbill) is a small tab projecting from the trailing edge of a wing. Typically it is set at a right angle to the pressure-side
Leading-edge slat
intended to operate within a wide range of speeds. Trailing-edge flap systems running along the trailing edge of the wing are common on all aircraft. Types
Kutta condition
that is applicable to solid bodies with sharp corners, such as the trailing edges of airfoils. It is named for German mathematician and aerodynamicist
Flight control surfaces
The Wright brothers used wing warping, a technique where the outer trailing edges of the wing were manipulated to control the roll. However, this technique
Supersonic airfoils
"biconvex airfoils" respectively), with very sharp leading and trailing edges. The sharp edges prevent the formation of a detached bow shock in front of the
ATA 100
581:Left Wing Trailing Edge, Outbd Aileron And Control Tab 582:Left Wing Trailing Edge Outbd Flap And Spoilers No1 - No4 583:Left Wing Trailing Edge, Inbd Aileron