Explore: Drag Reduction
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Source: The Open Library
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1A reassessment of heavy-duty truck aerodynamic design features and priorities
By Edwin J. Saltzman
“A reassessment of heavy-duty truck aerodynamic design features and priorities” Metadata:
- Title: ➤ A reassessment of heavy-duty truck aerodynamic design features and priorities
- Author: Edwin J. Saltzman
- Language: English
- Number of Pages: Median: 32
- Publisher: ➤ Available from NASA Center for AeroSpace Information - National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - Edwards, Calif - Hanover, Md
“A reassessment of heavy-duty truck aerodynamic design features and priorities” Subjects and Themes:
- Subjects: ➤ Trucks - Drag reduction - Research - Tractors - Aerodynamic drag - Experimentation - Aerodynamics - Tractor trailer combinations
Edition Identifiers:
- The Open Library ID: OL17591576M - OL17136010M - OL15556456M - OL19158918M - OL18137665M
- Online Computer Library Center (OCLC) ID: 42885469
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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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
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3Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness
By Stephen A. Whitmore
“Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness” Metadata:
- Title: ➤ Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness
- Author: Stephen A. Whitmore
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 2001
- Publish Location: ➤ Springfield, VA - Edwards, Calif
“Wind-tunnel investigations of blunt-body drug reduction using forebody surface roughness” Subjects and Themes:
- Subjects: Base flow - Wind tunnel tests - Aerodynamic drag - Drag reduction
Edition Identifiers:
- The Open Library ID: OL18160767M - OL16012016M - OL17601365M - OL18347098M
- Online Computer Library Center (OCLC) ID: 47969712
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4International Space Station
By Johnson, L.
“International Space Station” Metadata:
- Title: International Space Station
- Author: Johnson, L.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Marshall Space Flight Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Huntsville, Ala.] - Springfield, VA
“International Space Station” Subjects and Themes:
- Subjects: ➤ Aerodynamic drag - Drag reduction - International Space Station - Orbit decay - Tethering - Tetherlines
Edition Identifiers:
- The Open Library ID: OL18133293M - OL17700932M - OL17593140M
- Online Computer Library Center (OCLC) ID: 41226745
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS)
By Mohamed E. Eleshaky
“Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS)” Metadata:
- Title: ➤ Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS)
- Author: Mohamed E. Eleshaky
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“Design of 3-D nacelle near flat-plate wing using multiblock sensitivity analysis (ADOS)” Subjects and Themes:
- Subjects: Aircraft design - Design analysis - Drag reduction - Nacelles - Wing nacelle configuration
Edition Identifiers:
- The Open Library ID: OL15419482M - OL17078545M - OL18084619M
- Online Computer Library Center (OCLC) ID: 34608788
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
By Sheryll Goecke Powers
“Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers” Metadata:
- Title: ➤ Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers
- Author: Sheryll Goecke Powers
- Language: English
- Number of Pages: Median: 139
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Branch - Dryden Flight Research Facility
- Publish Date: 1986 - 1988
- Publish Location: ➤ Edwards, Cal - [Springfield, Va - [Washington, DC]
“Flight and wind-tunnel measurements showing base drag reduction provided by a trailing disk for high Reynolds number turbulent flow for subsonic and transonic Mach numbers” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Blunt bodies - Drag reduction - Trapped vortexes - Bodies of revolution - Mach number - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL15276247M - OL20985601M - OL18029606M
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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7On the use of external burning to reduce aerospace vehicle transonic drag
By Charles J. Trefny
“On the use of external burning to reduce aerospace vehicle transonic drag” Metadata:
- Title: ➤ On the use of external burning to reduce aerospace vehicle transonic drag
- Author: Charles J. Trefny
- Language: English
- Number of Pages: Median: 14
- Publisher: ➤ For sale by the National Technical Information Service - NASA
- Publish Date: 1990
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“On the use of external burning to reduce aerospace vehicle transonic drag” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Space vehicles - Drag (Aerodynamics) - Combustion - Turbojet engines - Drag reduction - Flame stability - Aerospace vehicles - Reaction kinetics - Aerodynamic drag - Hydrogen
Edition Identifiers:
- The Open Library ID: OL17630522M - OL16135223M
- Online Computer Library Center (OCLC) ID: 30712306
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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8Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
By W. S. Saric
“Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel” Metadata:
- Title: ➤ Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel
- Author: W. S. Saric
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Hybrid laminar flow control experiments in the NASA - Ames, 11-foot tunnel” Subjects and Themes:
- Subjects: ➤ Drag reduction - Surface roughness effects - Wind tunnel tests - Swept wings - Laminar boundary layer - Boundary layer control - Boundary layer transition - Turbulence effects
Edition Identifiers:
- The Open Library ID: OL15423184M - OL17796516M
- Online Computer Library Center (OCLC) ID: 35290580
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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9Effects of winglets on the drag of a low-aspect-ratio configuration
By Leigh Ann Smith
“Effects of winglets on the drag of a low-aspect-ratio configuration” Metadata:
- Title: ➤ Effects of winglets on the drag of a low-aspect-ratio configuration
- Author: Leigh Ann Smith
- Language: English
- Number of Pages: Median: 57
- Publisher: ➤ National Aeronautics and Space Administration - Langley Research Center
- Publish Date: 1996
- Publish Location: Hampton, Va - Washington, DC
“Effects of winglets on the drag of a low-aspect-ratio configuration” Subjects and Themes:
- Subjects: Drag reduction - Winglets
Edition Identifiers:
- The Open Library ID: OL21866680M - OL19005662M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10A method for the design of transonic flexible wings
By Leigh Ann Smith
“A method for the design of transonic flexible wings” Metadata:
- Title: ➤ A method for the design of transonic flexible wings
- Author: Leigh Ann Smith
- Language: English
- Number of Pages: Median: 38
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division - Langley Research Center - For sale by the National Technical Information Service]
- Publish Date: 1990 - 1991
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, DC]
“A method for the design of transonic flexible wings” Subjects and Themes:
- Subjects: ➤ Aerodynamics, Transonic - Aircraft design - Airplanes - Drag reduction - Transonic Aerodynamics - Wings
Edition Identifiers:
- The Open Library ID: OL15368333M - OL21335004M
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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11Drag reduction on circular cylinders by ejecting jet from rear stagnation region
By S. Atsuchi
“Drag reduction on circular cylinders by ejecting jet from rear stagnation region” Metadata:
- Title: ➤ Drag reduction on circular cylinders by ejecting jet from rear stagnation region
- Author: S. Atsuchi
- Language: English
- Publisher: ➤ Dept. of Mechanical Engineering, College of Engineering and Technology, Old Dominion University - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC - Norfolk, Va
“Drag reduction on circular cylinders by ejecting jet from rear stagnation region” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Drag reduction - Reynolds number - Pressure measurement - Stagnation point - Ejection - Finite volume method - Navier-Stokes equation - Circular cylinders - Algorithms - Injection
Edition Identifiers:
- The Open Library ID: OL17826956M - OL15491664M
- Online Computer Library Center (OCLC) ID: 39097177
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
By H. T. Nagamatsu
“Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction” Metadata:
- Title: ➤ Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction
- Author: H. T. Nagamatsu
- Language: English
- Publisher: NASA Langley Research Center
- Publish Date: 1983
- Publish Location: [Hampton, Va.?]
“Investigation to optimize the passive shock wave/boundary layer control for supercritical airfoil drag reduction” Subjects and Themes:
- Subjects: Boundary layer control - Aerofoils - Drag reduction - Supercritical wings - Shock waves
Edition Identifiers:
- The Open Library ID: OL16153613M - OL17635319M
- Online Computer Library Center (OCLC) ID: 173659340
Access and General Info:
- First Year Published: 1983
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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13Robust airfoil optimization to achieve consistent drag reduction over a mach range
By Wu Li
“Robust airfoil optimization to achieve consistent drag reduction over a mach range” Metadata:
- Title: ➤ Robust airfoil optimization to achieve consistent drag reduction over a mach range
- Author: Wu Li
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information
- Publish Date: 2001
- Publish Location: Hanover, MD - Hampton, Va
“Robust airfoil optimization to achieve consistent drag reduction over a mach range” Subjects and Themes:
- Subjects: ➤ Aerodynamic drag - Airfoils - Drag reduction - Mach number - Optimization - Robustness (Mathematics)
Edition Identifiers:
- The Open Library ID: OL16050922M - OL17633134M
- Online Computer Library Center (OCLC) ID: 54494222
Access and General Info:
- First Year Published: 2001
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14Feasibility of generating an "artificial" burst in a turbulent boundary layer
By Mohamed Gad-el-Hak
“Feasibility of generating an "artificial" burst in a turbulent boundary layer” Metadata:
- Title: ➤ Feasibility of generating an "artificial" burst in a turbulent boundary layer
- Author: Mohamed Gad-el-Hak
- Number of Pages: Median: 90
- Publisher: Langley Research Center
- Publish Date: 1986 - 1989
- Publish Location: Hampton, Va
“Feasibility of generating an "artificial" burst in a turbulent boundary layer” Subjects and Themes:
- Subjects: ➤ Artificial burst - Boundary layer control - Drag reduction - Skin friction - Suction - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL18930332M - OL20983893M
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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15Analysis and evaluation of an integrated laminar flow control propulsion system
By Theodore G. Keith
“Analysis and evaluation of an integrated laminar flow control propulsion system” Metadata:
- Title: ➤ Analysis and evaluation of an integrated laminar flow control propulsion system
- Author: Theodore G. Keith
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1993
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Analysis and evaluation of an integrated laminar flow control propulsion system” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Skin friction - Transport aircraft - Drag reduction - Friction reduction - Friction drag - Laminar boundary layer - Aerodynamic drag - Boundary layer control - Friction factor - Suction
Edition Identifiers:
- The Open Library ID: OL17683011M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Hydrodynamic aspects of shark scales
By William G. Raschi
“Hydrodynamic aspects of shark scales” Metadata:
- Title: ➤ Hydrodynamic aspects of shark scales
- Author: William G. Raschi
- Language: English
- Number of Pages: Median: 110
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service
- Publish Date: 1986
- Publish Location: ➤ Springfield, Va - [Washington, D.C.]
“Hydrodynamic aspects of shark scales” Subjects and Themes:
- Subjects: ➤ Sharks - Skin friction - Drag reduction - Hydrodynamics - Riblets - Morphology - Locomotion - Scales (Fishes)
Edition Identifiers:
- The Open Library ID: OL17724382M
- Online Computer Library Center (OCLC) ID: 15182495
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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17A concept for adaptive performance optimization on commercial transport aircraft
By Michael R. Jackson
“A concept for adaptive performance optimization on commercial transport aircraft” Metadata:
- Title: ➤ A concept for adaptive performance optimization on commercial transport aircraft
- Author: Michael R. Jackson
- Language: English
- Publisher: ➤ National Technical Information Service, distributor] - National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“A concept for adaptive performance optimization on commercial transport aircraft” Subjects and Themes:
- Subjects: ➤ Transport aircraft - Drag reduction - Monte Carlo method - Aerodynamic drag - Cambered wings - Commercial aircraft - Control surfaces - Adaptive control - Least squares method
Edition Identifiers:
- The Open Library ID: OL15423362M
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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18Use of riblets to obtain drag reduction on airfoils at high Reynolds number flows
By M. Khalid
“Use of riblets to obtain drag reduction on airfoils at high Reynolds number flows” Metadata:
- Title: ➤ Use of riblets to obtain drag reduction on airfoils at high Reynolds number flows
- Author: M. Khalid
- Number of Pages: Median: 19
- Publisher: ➤ National Aeronautical Establishment, National Research Council Canada
- Publish Date: 1988
- Publish Location: Ottawa
“Use of riblets to obtain drag reduction on airfoils at high Reynolds number flows” Subjects and Themes:
- Subjects: Airfoils - Riblets - Drag reduction
Edition Identifiers:
- The Open Library ID: OL18926699M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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19A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program
By Stephen A. Whitmore
“A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program” Metadata:
- Title: ➤ A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program
- Author: Stephen A. Whitmore
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Dryden Flight Research Center
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“A base drag reduction experiment on the X-33 Linear Aerospike SR-71 Experiment (LASRE) flight program” Subjects and Themes:
- Subjects: Aerodynamic drag - Flight tests - Drag measurement - Drag reduction
Edition Identifiers:
- The Open Library ID: OL15548948M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20High altitude towed glider
By Anthony J. Colozza
“High altitude towed glider” Metadata:
- Title: High altitude towed glider
- Author: Anthony J. Colozza
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“High altitude towed glider” Subjects and Themes:
- Subjects: ➤ Aerodynamic drag - Drag reduction - Gliders - High altitude - Remotely piloted Vehicles - Towed bodies
Edition Identifiers:
- The Open Library ID: OL15504936M
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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21Feasibility of generating an "artificial" burst in a turbulent boundary layer
By M. Gad-el-Hak
“Feasibility of generating an "artificial" burst in a turbulent boundary layer” Metadata:
- Title: ➤ Feasibility of generating an "artificial" burst in a turbulent boundary layer
- Author: M. Gad-el-Hak
- Language: English
- Number of Pages: Median: 50
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: [Washington, D.C.]
“Feasibility of generating an "artificial" burst in a turbulent boundary layer” Subjects and Themes:
- Subjects: ➤ Turbulent boundary layer - Mathematical models - Drag reduction - Vortex generators - Laminar flow - Bursts - Water tunnel tests - Vortices
Edition Identifiers:
- The Open Library ID: OL16122036M
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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22SAMID, an interactive system for aircraft drag minimization studies (mathematical models and methods)
By R. F. van den Dam
“SAMID, an interactive system for aircraft drag minimization studies (mathematical models and methods)” Metadata:
- Title: ➤ SAMID, an interactive system for aircraft drag minimization studies (mathematical models and methods)
- Author: R. F. van den Dam
- Number of Pages: Median: 58
- Publisher: National Aerospace Laboratory
- Publish Date: 1988
- Publish Location: Amsterdam, Netherlands
“SAMID, an interactive system for aircraft drag minimization studies (mathematical models and methods)” Subjects and Themes:
- Subjects: Drag reduction
Edition Identifiers:
- The Open Library ID: OL19165503M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
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- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
23Untersuchungen an einem transsonischen Profil mit 30 mm brieter Perforation/Kammer-Anordnung
By Paul Krogmann
“Untersuchungen an einem transsonischen Profil mit 30 mm brieter Perforation/Kammer-Anordnung” Metadata:
- Title: ➤ Untersuchungen an einem transsonischen Profil mit 30 mm brieter Perforation/Kammer-Anordnung
- Author: Paul Krogmann
- Number of Pages: Median: 48
- Publisher: DFVLR
- Publish Date: 1986
- Publish Location: Koln
“Untersuchungen an einem transsonischen Profil mit 30 mm brieter Perforation/Kammer-Anordnung” Subjects and Themes:
- Subjects: Boundary layer control - Drag reduction
Edition Identifiers:
- The Open Library ID: OL18998192M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Untersuchungen an einem transsonischen Profil mit 30 mm brieter Perforation/Kammer-Anordnung at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.