Explore: Wave Drag
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)
By Edwin J. Saltzman
“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Metadata:
- Title: ➤ In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)
- Author: Edwin J. Saltzman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Subjects and Themes:
- Subjects: ➤ X-29 aircraft - Wave drag - Lift - Airfoil profiles - Swept forward wings - Drag - Transonic speed
Edition Identifiers:
- The Open Library ID: OL18080007M - OL17008295M - OL15411782M
- Online Computer Library Center (OCLC) ID: 32938383
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.
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2Optimum shape of a blunt forebody in hypersonic flow
By L. Maestrello
“Optimum shape of a blunt forebody in hypersonic flow” Metadata:
- Title: ➤ Optimum shape of a blunt forebody in hypersonic flow
- Author: L. Maestrello
- Language: English
- Publisher: NASA Langley Research Center
- Publish Date: 1989
- Publish Location: Hampton, Va
“Optimum shape of a blunt forebody in hypersonic flow” Subjects and Themes:
- Subjects: ➤ Aerodynamic heating - Blunt bodies - Flow distribution - Forebodies - Hypersonic flow - Newton theory - Wave drag
Edition Identifiers:
- The Open Library ID: OL16122124M - OL17631952M
- Online Computer Library Center (OCLC) ID: 57932749
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:
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3Wave drag determination in the transonic full-potential flow code matrics
By J. Van der Vooren
“Wave drag determination in the transonic full-potential flow code matrics” Metadata:
- Title: ➤ Wave drag determination in the transonic full-potential flow code matrics
- Author: J. Van der Vooren
- Number of Pages: Median: 29
- Publisher: National Aerospace Laboratory
- Publish Date: 1990
- Publish Location: Amsterdam
“Wave drag determination in the transonic full-potential flow code matrics” Subjects and Themes:
- Subjects: Transonic flow - Wave drag - Finite volume method
Edition Identifiers:
- The Open Library ID: OL21378482M
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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4Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips
By Paul Kolodziej
“Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips” Metadata:
- Title: ➤ Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips
- Author: Paul Kolodziej
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Aerothermal performance constraints for hypervelocity small radius unswept leading edges and nosetips” Subjects and Themes:
- Subjects: ➤ Ablation - Heating - Aerothermodynamics - Wave drag - Thermal protection - Leading edges - Nose tips - Ceramics
Edition Identifiers:
- The Open Library ID: OL17128484M
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.
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Wave drag
In aeronautics, wave drag is a component of the aerodynamic drag on aircraft wings and fuselage, propeller blade tips and projectiles moving at transonic
Drag (physics)
of categorizing drag. Pressure drag and friction drag Profile drag and induced drag Vortex drag, wave drag and wake drag The pressure distribution acting
Parasitic drag
Parasitic drag, also known as profile drag, is a type of aerodynamic drag that acts on any object when the object is moving through a fluid. Parasitic drag is
Area rule
waves formed at these zones of sonic flow cause a sudden increase in drag, called wave drag. To reduce the number and strength of these shock waves,
Supercritical airfoil
British English) is an airfoil designed primarily to delay the onset of wave drag in the transonic speed range. Supercritical airfoils are characterized
Shock wave
extracted as work, and as a drag force on supersonic objects; shock waves are strongly irreversible processes. Shock waves can be: Normal At 90° (perpendicular)
Transonic
increase in drag from about Mach 0.8, and it is the fuel costs of the drag that typically limits the airspeed. Attempts to reduce wave drag can be seen
Wave-making resistance
Wave-making resistance or wave resistance is a form of drag that affects any object moving on a surface of a fluid, such as boats and ships moving on
Busemann biplane
which avoids the formation of N-type shock waves and thus does not create a sonic boom or the associated wave drag. However in its original form it does not
Sears–Haack body
The Sears–Haack body is the shape with the lowest theoretical wave drag in supersonic flow, for a slender solid body of revolution with a given body length