Explore: Yawing (aerodynamics
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Comparison of yaw characteristics of a single-engine airplane model with single-rotating and dual-rotating propellers
By Langley Aeronautical Laboratory
“Comparison of yaw characteristics of a single-engine airplane model with single-rotating and dual-rotating propellers” Metadata:
- Title: ➤ Comparison of yaw characteristics of a single-engine airplane model with single-rotating and dual-rotating propellers
- Author: ➤ Langley Aeronautical Laboratory
- Language: English
- Number of Pages: Median: 66
- Publisher: ➤ Langley Memorial Aeronautical Laboratory
- Publish Date: 1944
- Publish Location: Langley Field, VA
“Comparison of yaw characteristics of a single-engine airplane model with single-rotating and dual-rotating propellers” Subjects and Themes:
- Subjects: Yawing (Aerodynamics - Propellers, Aerial--Testing.
Edition Identifiers:
- The Open Library ID: OL58773933M
Access and General Info:
- First Year Published: 1944
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
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2Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube
By Langley Aeronautical Laboratory
“Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube” Metadata:
- Title: ➤ Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube
- Author: ➤ Langley Aeronautical Laboratory
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ Langley Memorial Aeronautical Laboratory
- Publish Date: 1945
- Publish Location: Langley Field, VA
“Effects of compressibility and large angles of yaw on pressure indicated by a total-pressure tube” Subjects and Themes:
- Subjects: Yawing (Aerodynamics - Compressibility - Aerodynamics--Research.
Edition Identifiers:
- The Open Library ID: OL58820099M
Access and General Info:
- First Year Published: 1945
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
Online Marketplaces
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3Formulas for propellers in yaw and charts on the side-force derivative
By Langley Aeronautical Laboratory
“Formulas for propellers in yaw and charts on the side-force derivative” Metadata:
- Title: ➤ Formulas for propellers in yaw and charts on the side-force derivative
- Author: ➤ Langley Aeronautical Laboratory
- Language: English
- Number of Pages: Median: 32
- Publisher: ➤ Langley Memorial Aeronautical Laboratory
- Publish Date: 1943
- Publish Location: Langley Field, VA
“Formulas for propellers in yaw and charts on the side-force derivative” Subjects and Themes:
- Subjects: Propellers, Aerial - Yawing (Aerodynamics - Aeronautics--Research.
Edition Identifiers:
- The Open Library ID: OL58839352M
Access and General Info:
- First Year Published: 1943
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
Online Marketplaces
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4Effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel
By Langley Aeronautical Laboratory
“Effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel” Metadata:
- Title: ➤ Effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel
- Author: ➤ Langley Aeronautical Laboratory
- Language: English
- Number of Pages: Median: 32
- Publisher: ➤ Langley Memorial Aeronautical Laboratory
- Publish Date: 1946
- Publish Location: Langley Field, VA
“Effect of lateral area on the lateral stability and control characteristics of an airplane as determined by tests of a model in the Langley free-flight tunnel” Subjects and Themes:
- Subjects: Yawing (Aerodynamics - Aerodynamics--Research.
Edition Identifiers:
- The Open Library ID: OL58819991M
Access and General Info:
- First Year Published: 1946
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
Online Marketplaces
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5Propellers in yaw
By Langley Aeronautical Laboratory
“Propellers in yaw” Metadata:
- Title: Propellers in yaw
- Author: ➤ Langley Aeronautical Laboratory
- Language: English
- Number of Pages: Median: 86
- Publisher: ➤ Langley Memorial Aeronautical Laboratory
- Publish Date: 1943
- Publish Location: Langley Field, VA
“Propellers in yaw” Subjects and Themes:
- Subjects: Propellers, Aerial - Yawing (Aerodynamics - Aeronautics--Research.
Edition Identifiers:
- The Open Library ID: OL58998071M
Access and General Info:
- First Year Published: 1943
- Is Full Text Available: Yes
- Is The Book Public: Yes
- Access Status: Public
Online Access
Online Borrowing:
- Borrowing from Open Library: Borrowing link
- Borrowing from Archive.org: Borrowing link
Online Marketplaces
Find Propellers in yaw at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Aircraft principal axes
is called yaw. A positive yawing motion moves the nose of the aircraft to the right. The rudder is the primary control of yaw. The term yaw was originally
Slip (aerodynamics)
an airplane in a slip is made to stall, it displays very little of the yawing tendency that causes a skidding stall to develop into a spin. A stalling
Spin (aerodynamics)
aircraft to roll, and the difference in drag causes the aircraft to continue yawing. The spin characteristics diagram shown in this section is typical of an
Tandem-rotor aircraft
configuration. Single-rotor helicopters need a mechanism to neutralize the yawing movement produced by the single large rotor. This is commonly accomplished
Skid (aerodynamics)
applied in order to bank the airplane, the ailerons also cause an adverse yaw of the airplane. For example, if the airplane is rolling clockwise (from
Model aircraft
Schuster, New York, 1967. ISBN 0671289918 OCLC 437094 Model Aircraft Aerodynamics, by Martin Simons, Swanley: Nexus Special Interests, 1999. 4th ed. ISBN 1854861905
Wind-turbine aerodynamics
application of wind turbines is to generate energy using the wind. Hence, the aerodynamics is a very important aspect of wind turbines. Like most machines, wind
Stall (fluid dynamics)
about its yaw axis is called a spin. A spin can occur if an aircraft is stalled and there is an asymmetric yawing moment applied to it. This yawing moment
Flight dynamics
deliberately "side-slipped" when landing in a cross-wind, as explained in slip (aerodynamics). The forces acting on space vehicles are of three types: propulsive
Dutch roll
forcing the lifting wing back, yawing the aircraft toward it. This yawing effect produced by rolling motion is known as adverse yaw. This has to be countered