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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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2In-flight transport performance optimization
By Glenn B. Gilyard
“In-flight transport performance optimization” Metadata:
- Title: ➤ In-flight transport performance optimization
- Author: Glenn B. Gilyard
- Language: English
- Number of Pages: Median: 15
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“In-flight transport performance optimization” Subjects and Themes:
- Subjects: ➤ Ailerons - Airplanes - Transport vehicles - Real time operation - Cambered wings - Wing loading - Flight tests - Optimization - Aerodynamic drag - L-1011 aircraft - Handling characteristics - Jet transports - Flight testing - Wings - Drag (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL18118712M - OL17125500M - OL17572312M - OL17697192M - OL18889777M
- Online Computer Library Center (OCLC) ID: 39824781
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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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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4IPAC--Inlet Performance Analysis Code
By Paul J. Barnhart
“IPAC--Inlet Performance Analysis Code” Metadata:
- Title: ➤ IPAC--Inlet Performance Analysis Code
- Author: Paul J. Barnhart
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“IPAC--Inlet Performance Analysis Code” Subjects and Themes:
- Subjects: ➤ Engine inlets - Inlet flow - Aerodynamic coefficients - Pressure recovery - Aerodynamic drag - Reliability analysis
Edition Identifiers:
- The Open Library ID: OL18115388M - OL17564997M - OL17123843M - OL15489478M
- Online Computer Library Center (OCLC) ID: 39289699
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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5International 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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6Reducing wind tunnel data requirements using neural networks
By James C. Ross
“Reducing wind tunnel data requirements using neural networks” Metadata:
- Title: ➤ Reducing wind tunnel data requirements using neural networks
- Author: James C. Ross
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Reducing wind tunnel data requirements using neural networks” Subjects and Themes:
- Subjects: ➤ Accuracy - Aerodynamic characteristics - Aerodynamic drag - Data reduction - Neural nets - Pitching moments - Wind tunnel models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17837960M - OL15542964M
- Online Computer Library Center (OCLC) ID: 40638566
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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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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8A novel potential viscous flow coupling technique for computing helicopter flow fields
By J. Michael Summa
“A novel potential viscous flow coupling technique for computing helicopter flow fields” Metadata:
- Title: ➤ A novel potential viscous flow coupling technique for computing helicopter flow fields
- Author: J. Michael Summa
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1990
- Publish Location: Moffett Field, Calif
“A novel potential viscous flow coupling technique for computing helicopter flow fields” Subjects and Themes:
- Subjects: ➤ Aerodynamic drag - Computational fluid dynamics - Feedback control - Flow distribution - Helicopters - Iteration - Potential flow - Rotary wings - Rotors - Velocity coupling - Velocity distribution
Edition Identifiers:
- The Open Library ID: OL17631923M - OL17725830M
- Online Computer Library Center (OCLC) ID: 63905506
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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9A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept
By Bernard Spencer
“A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” Metadata:
- Title: ➤ A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept
- Author: Bernard Spencer
- 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
“A study to determine methods of improving the subsonic performance of a proposed Personnel Launch System (PLS) concept” Subjects and Themes:
- Subjects: ➤ Launch vehicles - Lift drag ratio - Wind tunnel tests - Subsonic flow - Assured crew return vehicle - Angle of attack - Pitching moments - Lift - Aerodynamic drag - Aerodynamic configurations
Edition Identifiers:
- The Open Library ID: OL17106590M - OL17685249M
- Online Computer Library Center (OCLC) ID: 35281561
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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10Flight test of an adaptive configuration optimization system for transport aircraft
By Glenn B. Gilyard
“Flight test of an adaptive configuration optimization system for transport aircraft” Metadata:
- Title: ➤ Flight test of an adaptive configuration optimization system for transport aircraft
- Author: Glenn B. Gilyard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - Edwards, Calif
“Flight test of an adaptive configuration optimization system for transport aircraft” Subjects and Themes:
- Subjects: ➤ Adaptive control - Aerodynamic drag - Aircraft performance - Angle of attack - Cambered wings - Data acquisition - Flight tests - Transport aircraft
Edition Identifiers:
- The Open Library ID: OL17593117M - OL15542421M
- Online Computer Library Center (OCLC) ID: 42042457
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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11Study of potential aerodynamic benefits from spanwise blowing at wingtip
By Raymond E. Mineck
“Study of potential aerodynamic benefits from spanwise blowing at wingtip” Metadata:
- Title: ➤ Study of potential aerodynamic benefits from spanwise blowing at wingtip
- Author: Raymond E. Mineck
- 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
“Study of potential aerodynamic benefits from spanwise blowing at wingtip” Subjects and Themes:
- Subjects: ➤ Aerodynamic drag - Aerodynamics - Commercial aircraft - Lift - Navier-Stokes equation - Spanwise blowing - Subsonic speed - Swept wings - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15413573M - OL17791713M
- Online Computer Library Center (OCLC) ID: 33401866
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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12Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
By Jim A. Penland
“Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Metadata:
- Title: ➤ Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results
- Author: Jim A. Penland
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Invariance of hypersonic normal force coefficients with Reynolds number and determination of inviscid wave drag from laminar experimental results” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent boundary layer - Aerodynamic coefficients - Body-wing configurations - Reynolds number - Hypersonic forces - Hypersonic boundary layer - Aerodynamic drag - Hypersonic shock - Mach number
Edition Identifiers:
- The Open Library ID: OL17591848M - OL15548849M
- Online Computer Library Center (OCLC) ID: 42677545
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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13A Two element laminar flow airfoil optimized for cruise
By Gregory Glen Steen
“A Two element laminar flow airfoil optimized for cruise” Metadata:
- Title: ➤ A Two element laminar flow airfoil optimized for cruise
- Author: Gregory Glen Steen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Texas A&M University - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [College Station, TX?] - [Washington, DC - Springfield, Va
“A Two element laminar flow airfoil optimized for cruise” Subjects and Themes:
- Subjects: ➤ Aerodynamic configurations - Aerodynamic drag - Aircraft design - Airfoils - Cruising flight - Laminar flow - Lift - Lift drag ratio - Wind tunnel tests - Wings
Edition Identifiers:
- The Open Library ID: OL15414633M - OL17792073M
- Online Computer Library Center (OCLC) ID: 34053955
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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14Robust 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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15A wind tunnel investigation of the steady aerodynamic forces and moments on partially streamlined motorcycles
By Kevin R. Cooper
“A wind tunnel investigation of the steady aerodynamic forces and moments on partially streamlined motorcycles” Metadata:
- Title: ➤ A wind tunnel investigation of the steady aerodynamic forces and moments on partially streamlined motorcycles
- Author: Kevin R. Cooper
- Number of Pages: Median: 19
- Publisher: ➤ National Research Council Canada, National Aeronautical Establishment
- Publish Date: 1973
- Publish Location: Ottawa
“A wind tunnel investigation of the steady aerodynamic forces and moments on partially streamlined motorcycles” Subjects and Themes:
- Subjects: Aerodynamic drag - Motorcycles
Edition Identifiers:
- The Open Library ID: OL21499334M
Access and General Info:
- First Year Published: 1973
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Analysis 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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17Aerodynamics of heat exchangers for high-altitude aircraft
By Mark Drela
“Aerodynamics of heat exchangers for high-altitude aircraft” Metadata:
- Title: ➤ Aerodynamics of heat exchangers for high-altitude aircraft
- Author: Mark Drela
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Aerodynamics of heat exchangers for high-altitude aircraft” Subjects and Themes:
- Subjects: ➤ Heat exchangers - Aerodynamic heat transfer - Convective heat transfer - High altitude - Airfoil profiles - Inlet airframe configurations - Aerodynamic drag - Aircraft design
Edition Identifiers:
- The Open Library ID: OL15504835M
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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18Demonstration of the coast-down technique for determining train resistances
By Bain Dayman
“Demonstration of the coast-down technique for determining train resistances” Metadata:
- Title: ➤ Demonstration of the coast-down technique for determining train resistances
- Author: Bain Dayman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Jet Propulsion Laboratory, California Institute of Technology
- Publish Date: 1983
- Publish Location: Pasadena, Calif
“Demonstration of the coast-down technique for determining train resistances” Subjects and Themes:
- Subjects: ➤ Energy consumption - Railroads - Aerodynamic drag - Rolling contact loads - Cost estimates - Aerodynamics
Edition Identifiers:
- The Open Library ID: OL16154739M
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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19Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
By Milton Lamb
“Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” Metadata:
- Title: ➤ Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport
- Author: Milton Lamb
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Branch
- Publish Date: 1986
- Publish Location: ➤ Washington, D.C - Springfield, Va
“Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport” Subjects and Themes:
- Subjects: ➤ Nacelles - Skin friction - Pylons - System effectiveness - Wind tunnel tests - Testing - Airplanes - Aerodynamic drag - Transonic planes - Wings
Edition Identifiers:
- The Open Library ID: OL16152786M
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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20Preliminary wind tunnel tests on the influence of ground board length on the aerodynamic drag of simple commmercial vehicle models
By Kevin P. Garry
“Preliminary wind tunnel tests on the influence of ground board length on the aerodynamic drag of simple commmercial vehicle models” Metadata:
- Title: ➤ Preliminary wind tunnel tests on the influence of ground board length on the aerodynamic drag of simple commmercial vehicle models
- Author: Kevin P. Garry
- Number of Pages: Median: 14
- Publisher: ➤ College of Aeronautics, Cranfield Institute of Technology
- Publish Date: 1986
- Publish Location: Cranfield, U.K
“Preliminary wind tunnel tests on the influence of ground board length on the aerodynamic drag of simple commmercial vehicle models” Subjects and Themes:
- Subjects: Wind tunnel tests - Aerodynamic drag
Edition Identifiers:
- The Open Library ID: OL20984011M
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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21A summary of the scale model wind tunnel measurements and full scale surface pressure tests on the Leyland T45 and DAF3300 vehicles used for the TRRL spray dispersion programme
By Kevin P. Garry
“A summary of the scale model wind tunnel measurements and full scale surface pressure tests on the Leyland T45 and DAF3300 vehicles used for the TRRL spray dispersion programme” Metadata:
- Title: ➤ A summary of the scale model wind tunnel measurements and full scale surface pressure tests on the Leyland T45 and DAF3300 vehicles used for the TRRL spray dispersion programme
- Author: Kevin P. Garry
- Number of Pages: Median: 25
- Publisher: ➤ College of Aeronautics, Cranfield Institute of Technology
- Publish Date: 1987
- Publish Location: Cranfield [U.K.]
“A summary of the scale model wind tunnel measurements and full scale surface pressure tests on the Leyland T45 and DAF3300 vehicles used for the TRRL spray dispersion programme” Subjects and Themes:
- Subjects: Spray dispersion - Streamlining - Aerodynamic drag
Edition Identifiers:
- The Open Library ID: OL19247189M
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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22Model engine performance measurement from force balance instrumentation
By Robert J. Jeracki
“Model engine performance measurement from force balance instrumentation” Metadata:
- Title: ➤ Model engine performance measurement from force balance instrumentation
- Author: Robert J. Jeracki
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - [Cleveland, Ohio]
“Model engine performance measurement from force balance instrumentation” Subjects and Themes:
- Subjects: ➤ Thrust - Fan blades - Aerodynamic drag - Turbofan engines - Ducted fans - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL15544458M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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23A 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
Online Access
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24Neural network prediction of new aircraft design coefficients
By Magnus Nørgaard
“Neural network prediction of new aircraft design coefficients” Metadata:
- Title: ➤ Neural network prediction of new aircraft design coefficients
- Author: Magnus Nørgaard
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Neural network prediction of new aircraft design coefficients” Subjects and Themes:
- Subjects: ➤ Lift - Neural nets - Lift drag ratio - Wind tunnel tests - Aerodynamic drag - Moments of inertia - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15503737M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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25An empirical correction method for improving off-axes response prediction in component type flight mechanics helicopter models
By M. Hossein Mansur
“An empirical correction method for improving off-axes response prediction in component type flight mechanics helicopter models” Metadata:
- Title: ➤ An empirical correction method for improving off-axes response prediction in component type flight mechanics helicopter models
- Author: M. Hossein Mansur
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Moffett Field, CA - [Springfield, Va
“An empirical correction method for improving off-axes response prediction in component type flight mechanics helicopter models” Subjects and Themes:
- Subjects: ➤ Lift - Low pass filters - Models - Aerodynamic drag - Correction - AH-64 helicopter
Edition Identifiers:
- The Open Library ID: OL15542926M
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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26Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D
By C. L. Rumsey
“Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D” Metadata:
- Title: ➤ Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D
- Author: C. L. Rumsey
- 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
“Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D” Subjects and Themes:
- Subjects: Turbulence models - Aerodynamic drag - Body-wing configurations - Computational grids - Multiblock grids
Edition Identifiers:
- The Open Library ID: OL16046883M
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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27Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight
By G. H. Gaonkar
“Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” Metadata:
- Title: ➤ Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight
- Author: G. H. Gaonkar
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - Florida Atlantic University, Dept. of Mechanical Engineering, College of Engineering
- Publish Date: 1994
- Publish Location: ➤ Boca Raton, FL - Springfield, Va - [Washington, DC
“Sensitivity of lag-damping correlations to structural and aerodynamic approximations of isolated experimental rotors in forward flight” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aerodynamic drag - Wakes - Aerodynamic stalling - Torsional vibration - Aeroelasticity - Aerodynamic stability
Edition Identifiers:
- The Open Library ID: OL17029328M
- Online Computer Library Center (OCLC) ID: 32035217
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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28Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?
By J. W. Slooff
“Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?” Metadata:
- Title: ➤ Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?
- Author: J. W. Slooff
- Number of Pages: Median: 24
- Publisher: AGARD
- Publish Date: 1986
- Publish Location: Neuilly sur Seine, France
“Aircraft drag prediction and reduction: computational drag analyses and minimization; mission impossible?” Subjects and Themes:
- Subjects: ➤ Skin friction - Boundary layers - Aerodynamic drag - Turbulence - External stores - Laminar flow - Nacelles
Edition Identifiers:
- The Open Library ID: OL19987104M
Author's Alternative Names:
"Johannes W. Slooff", "Joop Slooff" and "J.W. Slooff"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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29A 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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30A preliminary design study of supersonic through-flow fan inlets
By Paul J. Barnhart
“A preliminary design study of supersonic through-flow fan inlets” Metadata:
- Title: ➤ A preliminary design study of supersonic through-flow fan inlets
- Author: Paul J. Barnhart
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1988
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“A preliminary design study of supersonic through-flow fan inlets” Subjects and Themes:
- Subjects: ➤ Inlet flow - Aerodynamic drag - Engine design - Turbofan engines - Supersonic flow - Mach number
Edition Identifiers:
- The Open Library ID: OL15407464M
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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31Simulated rarefied entry of the Galileo probe into the atmosphere of Jupiter
By Brian L. Haas
“Simulated rarefied entry of the Galileo probe into the atmosphere of Jupiter” Metadata:
- Title: ➤ Simulated rarefied entry of the Galileo probe into the atmosphere of Jupiter
- Author: Brian L. Haas
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1993
- Publish Location: ➤ [Springfield, Va - Washington, DC
“Simulated rarefied entry of the Galileo probe into the atmosphere of Jupiter” Subjects and Themes:
- Subjects: ➤ Rarefied gas dynamics - Computerized simulation - Atmospheric entry - Galileo probe - Monte Carlo method - Aerodynamic drag - Jupiter atmosphere - Aerobraking - Flow characteristics
Edition Identifiers:
- The Open Library ID: OL15411444M
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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32High 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
Online Access
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33A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept
By Bandu N. Pamadi
“A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept” Metadata:
- Title: ➤ A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept
- Author: Bandu N. Pamadi
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“A simple analytical aerodynamic model of Langley winged-cone aerospace plane concept” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Mathematical models - Angle of attack - Pitching moments - Lift - Aerodynamic drag - Hypersonic aircraft - Aerospace planes - Mach number
Edition Identifiers:
- The Open Library ID: OL15403126M
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:
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34Control of oscillatory forces on a circular cylinder by rotation
By Yuh-Roung Ou
“Control of oscillatory forces on a circular cylinder by rotation” Metadata:
- Title: ➤ Control of oscillatory forces on a circular cylinder by rotation
- Author: Yuh-Roung Ou
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Enginering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1991
- Publish Location: Hampton, Va - [Springfield, Va
“Control of oscillatory forces on a circular cylinder by rotation” Subjects and Themes:
- Subjects: ➤ Circular cylinders - Rotating cylinders - Oscillations - Aerodynamic drag - Rotation - Optimal control
Edition Identifiers:
- The Open Library ID: OL17683185M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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35A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies
By M. H. L. Hounjet
“A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies” Metadata:
- Title: ➤ A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies
- Author: M. H. L. Hounjet
- Number of Pages: Median: 39
- Publisher: National Aerospace Laboratory
- Publish Date: 1985
- Publish Location: Amsterdam
“A method to calculate steady and unsteady potential flow about fixed and rotating lifting and nonlifting bodies” Subjects and Themes:
- Subjects: ➤ Panel method (Fluid dynamics) - Aerodynamic drag - Wakes - Wind turbines - Wing oscillations - Rotor blades
Edition Identifiers:
- The Open Library ID: OL19001122M
Access and General Info:
- First Year Published: 1985
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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36Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2
By A. K. Sreekanth
“Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2” Metadata:
- Title: ➤ Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2
- Author: A. K. Sreekanth
- Number of Pages: Median: 46
- Publisher: [Institute of Aerophysics]
- Publish Date: 1961
- Publish Location: [Downsview, Ont.]
“Drag measurements of circular cylinders and spheres in the transition regime at a Mach number of 2” Subjects and Themes:
- Subjects: Aerodynamic drag - Drag measurement - Transition flow
Edition Identifiers:
- The Open Library ID: OL20985451M
Access and General Info:
- First Year Published: 1961
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2
By A. K. Sreekanth
“Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2” Metadata:
- Title: ➤ Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2
- Author: A. K. Sreekanth
- Number of Pages: Median: 46
- Publisher: Institute of Aerophysics
- Publish Date: 1961
- Publish Location: [Downsview, Ont.]
“Drag measurements on circular cylinders and spheres in the transition regime at a Mach number of 2” Subjects and Themes:
- Subjects: Aerodynamic drag - Drag measurement - Transition flow
Edition Identifiers:
- The Open Library ID: OL20897686M
Access and General Info:
- First Year Published: 1961
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Drag (physics)
measured by the Reynolds number. Examples of drag include: Net aerodynamic or hydrodynamic force: Drag acting opposite to the direction of movement of
Lift-to-drag ratio
lift-to-drag ratio (or L/D ratio) is the lift generated by an aerodynamic body such as an aerofoil or aircraft, divided by the aerodynamic drag caused
Lift-induced drag
Lift-induced drag, induced drag, vortex drag, or sometimes drag due to lift, in aerodynamics, is an aerodynamic drag force that occurs whenever a moving
Drag reduction system
In motor racing, the drag reduction system (DRS) is a form of driver-adjustable bodywork aimed at reducing aerodynamic drag in order to increase top speed
Automobile drag coefficient
into consideration the automobile drag coefficient in addition to the other performance characteristics. Aerodynamic drag increases with the square of speed;
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
Aerodynamics
eighteenth century, although observations of fundamental concepts such as aerodynamic drag were recorded much earlier. Most of the early efforts in aerodynamics
Drag coefficient
object will have less aerodynamic or hydrodynamic drag. The drag coefficient is always associated with a particular surface area. The drag coefficient of any
Skin friction drag
Skin friction drag or viscous drag is a type of aerodynamic or hydrodynamic drag, which is resistant force exerted on an object moving in a fluid. Skin
Kammback
cut off with a vertical or near-vertical surface. A Kammback reduces aerodynamic drag, thus improving efficiency and reducing fuel consumption, while maintaining