Explore: Dynamic Pressure
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Books Results
Source: The Open Library
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Search results from The Open Library
1User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
By Ronald H. Soeder
“User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Metadata:
- Title: ➤ User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel
- Author: Ronald H. Soeder
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1992 - 1995
- Publish Location: ➤ [Washington, DC - [Springfield, Va - [Washington, DC] - Springfield, Va
“User manual for NASA Lewis 10- by 10-Foot Supersonic Wind Tunnel” Subjects and Themes:
- Subjects: ➤ Supersonic wind tunnels - Performance tests - Dynamic pressure - User manuals (Computer programs) - Reynolds number - Wind tunnel tests - Mach number
Edition Identifiers:
- The Open Library ID: OL14687584M - OL17796406M - OL15425389M - OL17677053M
- Online Computer Library Center (OCLC) ID: 35268400
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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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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2Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
By Zachary T. Applin
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Metadata:
- Title: ➤ Pressure distributions from subsonic tests of a NACA 0012 semispan wing model
- Author: Zachary T. Applin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: Hampton, Va - [Springfield, Va
“Pressure distributions from subsonic tests of a NACA 0012 semispan wing model” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Airfoil profiles - Dynamic pressure - Free flow - Pressure distribution - Semispan models - Subsonic speed - Unswept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15421506M - OL17794166M
- Online Computer Library Center (OCLC) ID: 35231688
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.
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3Summary report of the orbital X-34 wing static aeroelastic study
By Ramadas K. Prabhu
“Summary report of the orbital X-34 wing static aeroelastic study” Metadata:
- Title: ➤ Summary report of the orbital X-34 wing static aeroelastic study
- Author: Ramadas K. Prabhu
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Science Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Summary report of the orbital X-34 wing static aeroelastic study” Subjects and Themes:
- Subjects: ➤ Inviscid flow - Computational fluid dynamics - Free flow - X-34 reusable launch vehicle - Aerodynamic characteristics - Flexibility - Dynamic pressure - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL17607405M - OL16030672M
- Online Computer Library Center (OCLC) ID: 50133893
Access and General Info:
- First Year Published: 2001
- 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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4Motion of the heliospheric termination shock at high heliographic latitude
By Aaron Barnes
“Motion of the heliospheric termination shock at high heliographic latitude” Metadata:
- Title: ➤ Motion of the heliospheric termination shock at high heliographic latitude
- Author: Aaron Barnes
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Motion of the heliospheric termination shock at high heliographic latitude” Subjects and Themes:
- Subjects: ➤ Asymmetry - Heliosphere - Solar wind - Dynamic pressure - Particle acceleration - Cosmic rays - Magnetohydrodynamics
Edition Identifiers:
- The Open Library ID: OL17837215M - OL15498391M
- Online Computer Library Center (OCLC) ID: 39725927
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.
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5A preliminary look at techniques used to obtain airdata from flight at high angles of attack
By Timothy R. Moes
“A preliminary look at techniques used to obtain airdata from flight at high angles of attack” Metadata:
- Title: ➤ A preliminary look at techniques used to obtain airdata from flight at high angles of attack
- Author: Timothy R. Moes
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“A preliminary look at techniques used to obtain airdata from flight at high angles of attack” Subjects and Themes:
- Subjects: ➤ Static pressure - F-18 aircraft - Calibrating - Sideslip - Angle of attack - Attitude gyros - Aerodynamics - Dynamic pressure - Accelerometers
Edition Identifiers:
- The Open Library ID: OL15405589M
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.
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6Method for experimental determination of flutter speed by parameter identification
By E. Nissim
“Method for experimental determination of flutter speed by parameter identification” Metadata:
- Title: ➤ Method for experimental determination of flutter speed by parameter identification
- Author: E. Nissim
- Language: English
- Number of Pages: Median: 40
- 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: ➤ [Washington, D.C.] - Springfield, VA
“Method for experimental determination of flutter speed by parameter identification” Subjects and Themes:
- Subjects: ➤ Flutter (Aerodynamics) - Parameter identification - Dynamic pressure - Mathematical models - Aeroelasticity - Flutter - Flight tests
Edition Identifiers:
- The Open Library ID: OL16123560M
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.
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7Pressure probe designs for dynamic pressure measurements in a supersonic flow field
By A. Robert Porro
“Pressure probe designs for dynamic pressure measurements in a supersonic flow field” Metadata:
- Title: ➤ Pressure probe designs for dynamic pressure measurements in a supersonic flow field
- Author: A. Robert Porro
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Pressure probe designs for dynamic pressure measurements in a supersonic flow field” Subjects and Themes:
- Subjects: ➤ Flow measurement - Supersonic wind tunnels - Dynamic pressure - Wind tunnel tests - Pressure sensors - Flow distribution
Edition Identifiers:
- The Open Library ID: OL16035831M
Access and General Info:
- First Year Published: 2001
- 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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8Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel
By D. M. Schuster
“Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel” Metadata:
- Title: ➤ Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel
- Author: D. M. Schuster
- Language: English
- Publisher: ➤ Available from NASA Center for AeroSpace Information (CASI) - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2001
- Publish Location: Hampton, Va - Hanover, MD
“Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel” Subjects and Themes:
- Subjects: ➤ Static pressure - Viscous flow - Transonic wind tunnels - Dynamic pressure - Wind tunnel tests - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL16028983M
Access and General Info:
- First Year Published: 2001
- 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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9Demodulation system for fiber optic Bragg grating dynamic pressure sensing
By John D. Lekki
“Demodulation system for fiber optic Bragg grating dynamic pressure sensing” Metadata:
- Title: ➤ Demodulation system for fiber optic Bragg grating dynamic pressure sensing
- Author: John D. Lekki
- Language: English
- Publisher: ➤ Available from NASA Center for Aerospace Information - National Aeronautics and Space Administration, Glenn Research Center
- Publish Date: 2001
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Demodulation system for fiber optic Bragg grating dynamic pressure sensing” Subjects and Themes:
- Subjects: ➤ Bragg gratings - Dynamic pressure - Pressure sensors - Demodulation - Fiber optics - Interferometry
Edition Identifiers:
- The Open Library ID: OL16035766M
Access and General Info:
- First Year Published: 2001
- 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
Dynamic pressure
In fluid dynamics, dynamic pressure (denoted by q or Q and sometimes called velocity pressure) is the quantity defined by: q = 1 2 ρ u 2 {\displaystyle
Max q
The max q, or maximum dynamic pressure, condition is the point when an aerospace vehicle's atmospheric flight reaches the maximum difference between the
Bernoulli's principle
pressure head) and p0 = p + q is the stagnation pressure (the sum of the static pressure p and dynamic pressure q). The constant in the Bernoulli equation
Stagnation pressure
equal to the dynamic pressure and static pressure combined. In compressible flows, stagnation pressure is also equal to total pressure as well, provided
Pressure measurement
dynamic pressures; this measurement is called the total pressure or stagnation pressure. Since dynamic pressure is referenced to static pressure, it is
Pressure
distributed. Gauge pressure (also spelled gage pressure) is the pressure relative to the ambient pressure. Various units are used to express pressure. Some of these
Pitot tube
static pressure as well it can be determined by the use of Bernoulli's equation which states: Stagnation pressure = static pressure + dynamic pressure Which
Static pressure
static pressure refers to a term in Bernoulli's equation written words as static pressure + dynamic pressure = total pressure. Since pressure measurements
Drag equation
P_{\rm {D}}A} where PD is the pressure exerted by the fluid on area A. Here the pressure PD is referred to as dynamic pressure due to the kinetic energy of
Water Resistant mark
properties of water and seawater, rapidly changing water pressure and temperature, as well as dynamic mechanical stresses encountered by a watch. Every "diver's"