Explore: Cavities (airplanes)
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AI-Generated Overview About “cavities-%28airplanes%29”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds
By J. E. Rossiter
“Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds” Metadata:
- Title: ➤ Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds
- Author: J. E. Rossiter
- Language: English
- Number of Pages: Median: 32
- Publisher: H.M.S.O.
- Publish Date: 1967
- Publish Location: London
“Wind-tunnel experiments on the flow over rectangular cavities at subsonic and transonic speeds” Subjects and Themes:
- Subjects: Cavities (Airplanes) - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL5580019M
- Library of Congress Control Number (LCCN): 67094055
Access and General Info:
- First Year Published: 1967
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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2Three-dimensional cavity flow fields at subsonic and transonic speeds
By Elizabeth B. Plentovich
“Three-dimensional cavity flow fields at subsonic and transonic speeds” Metadata:
- Title: ➤ Three-dimensional cavity flow fields at subsonic and transonic speeds
- Author: Elizabeth B. Plentovich
- Language: English
- Number of Pages: Median: 80
- Publisher: ➤ Langley Research Center - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - National Technical Information Service, distributor]
- Publish Date: 1990
- Publish Location: ➤ Hampton, Va - Washington, DC - [Springfield, Va
“Three-dimensional cavity flow fields at subsonic and transonic speeds” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Aerodynamics, Transonic - Cavities (Airplanes) - Cavity flow - Statistics - Transonic Aerodynamics
Edition Identifiers:
- The Open Library ID: OL17112322M - OL15396312M - OL18071129M - OL21333657M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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3Flow-induced resonance of screen-covered cavities
By Paul T. Soderman
“Flow-induced resonance of screen-covered cavities” Metadata:
- Title: ➤ Flow-induced resonance of screen-covered cavities
- Author: Paul T. Soderman
- Language: English
- Number of Pages: Median: 42
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Ames Research Center - For sale by the National Technical Information Service]
- Publish Date: 1990
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va - [Washington, DC]
“Flow-induced resonance of screen-covered cavities” Subjects and Themes:
- Subjects: Cavities (Airplanes) - Cavity resonance - Resonance
Edition Identifiers:
- The Open Library ID: OL21333961M - OL18035049M - OL15299721M
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:
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4Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
By A. B. Blair
“Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate” Metadata:
- Title: ➤ Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate
- Author: A. B. Blair
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service - Langley Research Center
- Publish Date: 1986
- Publish Location: ➤ Hampton, Va - Washington, D.C - Springfield, Va
“Supersonic axial-force characteristics of a rectangular-box cavity with various length-to-depth ratios in a flat plate” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Supersonic - Cavitation flow - Cavities (Airplanes) - Cavity flow - Flat plates - Flow distribution - Flow visualization - Supersonic Aerodynamics - Supersonics - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL19986377M - OL18290608M - OL17727208M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Solution of the Navier-Stokes equations for a driven cavity
By B. D. Semeraro
“Solution of the Navier-Stokes equations for a driven cavity” Metadata:
- Title: ➤ Solution of the Navier-Stokes equations for a driven cavity
- Author: B. D. Semeraro
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration
- Publish Date: 1991
- Publish Location: [Washington, D.C.?
“Solution of the Navier-Stokes equations for a driven cavity” Subjects and Themes:
- Subjects: Numerical solutions - Cavities (Airplanes) - Navier-Stokes equations
Edition Identifiers:
- The Open Library ID: OL18066955M - OL15390710M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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6Landing gear and cavity noise prediction
By Donald B. Bliss
“Landing gear and cavity noise prediction” Metadata:
- Title: ➤ Landing gear and cavity noise prediction
- Author: Donald B. Bliss
- Language: English
- Number of Pages: Median: 52
- Publisher: ➤ for sale by the National Technical Information Service - U.S. National Aeronautics and Space Administration
- Publish Date: 1976
- Publish Location: Washington - Springfield, Va
“Landing gear and cavity noise prediction” Subjects and Themes:
- Subjects: Airplanes - Noise - Cavities (Airplanes)
Edition Identifiers:
- The Open Library ID: OL17515981M - OL17645619M
Access and General Info:
- First Year Published: 1976
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing
By M. D. Dobson
“Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing” Metadata:
- Title: ➤ Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing
- Author: M. D. Dobson
- Language: English
- Number of Pages: Median: 22
- Publisher: H.M. Stationery Off.
- Publish Date: 1970
- Publish Location: London
“Tests at a mach number of 2.0 on a rectangular, twin-duct air intake with variable geometry, situated in the flow field of a slender wing” Subjects and Themes:
- Subjects: Cavities (Airplanes) - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL4370742M
- Library of Congress Control Number (LCCN): 78552764
Access and General Info:
- First Year Published: 1970
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Supersonic aerodynamic interference effects of store separation
By Oktay Baysal
“Supersonic aerodynamic interference effects of store separation” Metadata:
- Title: ➤ Supersonic aerodynamic interference effects of store separation
- Author: Oktay Baysal
- Language: English
- Publisher: ➤ Dept. of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University
- Publish Date: 1987
- Publish Location: Norfolk, Va
“Supersonic aerodynamic interference effects of store separation” Subjects and Themes:
- Subjects: Aerodynamics - Cavities (Airplanes) - High-speed aeronautics - Mathematical models
Edition Identifiers:
- The Open Library ID: OL15277222M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9An unsteady time asymptotic flow in the square driven cavity
By John W. Goodrich
“An unsteady time asymptotic flow in the square driven cavity” Metadata:
- Title: ➤ An unsteady time asymptotic flow in the square driven cavity
- Author: John W. Goodrich
- Language: English
- Number of Pages: Median: 10
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“An unsteady time asymptotic flow in the square driven cavity” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Cavities - Incompressible flow - Asymptotic methods - Research - Cavities (Airplanes) - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL16127958M
Access and General Info:
- First Year Published: 1990
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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10Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
By Elizabeth B. Plentovich
“Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Metadata:
- Title: ➤ Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds
- Author: Elizabeth B. Plentovich
- Language: English
- Number of Pages: Median: 51
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“Effects of yaw angle and Reynolds number on rectangular-box cavities at subsonic and transonic speeds” Subjects and Themes:
- Subjects: ➤ Aerodynamic load - Aerodynamics, Transonic - Cavities - Cavities (Airplanes) - Flow distribution - High Reynolds number - Mach number - Pressure distribution - Reynolds number - Subsonic flow - Transonic Aerodynamics - Transonic flow - Turbulent boundary layer - Yaw - Yawing (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16135213M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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11Evaluation of a vortex model of turbulent cavity flow
By Jay C Hardin
“Evaluation of a vortex model of turbulent cavity flow” Metadata:
- Title: ➤ Evaluation of a vortex model of turbulent cavity flow
- Author: Jay C Hardin
- Language: English
- Number of Pages: Median: 44
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1979
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Evaluation of a vortex model of turbulent cavity flow” Subjects and Themes:
- Subjects: Unsteady flow (Aerodynamics) - Cavities (Airplanes)
Edition Identifiers:
- The Open Library ID: OL14932463M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds
By Robert L. Stallings
“Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds” Metadata:
- Title: ➤ Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds
- Author: Robert L. Stallings
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Measurements of forces, moments, and pressures on a generic store separating from a box cavity at supersonic speeds” Subjects and Themes:
- Subjects: Cavities (Airplanes) - Aerodynamic load
Edition Identifiers:
- The Open Library ID: OL15354752M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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13Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel
By M. B. Tracy
“Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel” Metadata:
- Title: ➤ Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel
- Author: M. B. Tracy
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Characterization of cavity flow fields using pressure data obtained in the Langley 0.3-Meter Transonic Cryogenic Tunnel” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL14690127M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Uncontrolled decompression
too fast for air to escape safely from the lungs and other air-filled cavities in the body such as the sinuses and eustachian tubes, typically resulting
Electrician
electrical infrastructure. Electricians may also specialize in wiring ships, airplanes, and other mobile platforms, as well as data and cable lines. Electricians
Boeing Pelican
solid ground, then enters descent to arrive at an airport like other airplanes. This capability differentiates the aircraft from some previously built
Vestibule
boots, packs and small equipment In general, vestibule is a small space or cavity at the beginning of a canal. The vulval vestibule is a part of the vulva
FG 42
into battery by two lugs on the bolt head which recessed into appropriate cavities machined into the receiver walls. Owing to its main intended use by paratroopers
Barotrauma
between IEBt vs IEDCS is doubtful. The sinuses, like other air-filled cavities, are susceptible to barotrauma if their openings become obstructed. This
Aft pressure bulkhead
more weight. Patents have been filed that propose deliberately creating cavities within the rear bulkhead with the purpose of providing more usable cabin
Helmholtz resonance
pattern; this is called a resistive sheet; a series of so-called honeycomb cavities (holes with a honeycomb shape, but in fact only their volume matters).
MEMS magnetic field sensor
localize the flaw. When we breathe, the nerves and muscles of our thoracic cavity create a weak magnetic field. Magnetometers based on piezoelectric resonators
Sprue (manufacturing)
fabricate additional parts, such as railings on model ships, antenna wires on airplanes, or greebles on fictional spacecraft. Sprues in model kits often include