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Source: The Open Library
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Search results from The Open Library
1Microfabricated ice-detection sensor
By Russell G. DeAnna
“Microfabricated ice-detection sensor” Metadata:
- Title: ➤ Microfabricated ice-detection sensor
- Author: Russell G. DeAnna
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Microfabricated ice-detection sensor” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL18121070M - OL17579553M - OL17129564M - OL15503670M
- Online Computer Library Center (OCLC) ID: 41031153
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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2Two-dimensional high-lift aerodynamic optimization using neural networks
By Roxana M. Greenman
“Two-dimensional high-lift aerodynamic optimization using neural networks” Metadata:
- Title: ➤ Two-dimensional high-lift aerodynamic optimization using neural networks
- Author: Roxana M. Greenman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - Moffett Field, Calif
“Two-dimensional high-lift aerodynamic optimization using neural networks” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Computers - Navier-Stokes equation - Lift - Neural nets - Airfoils - Aerodynamic configurations - Angle of attack - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL17129961M - OL17580142M - OL18132744M - OL15542052M
- Online Computer Library Center (OCLC) ID: 41151565
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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3Validation of vortex-lattice method for loads on wings in lift-generated wakes
By Vernon J. Rossow
“Validation of vortex-lattice method for loads on wings in lift-generated wakes” Metadata:
- Title: ➤ Validation of vortex-lattice method for loads on wings in lift-generated wakes
- Author: Vernon J. Rossow
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - [National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - Washington, DC
“Validation of vortex-lattice method for loads on wings in lift-generated wakes” Subjects and Themes:
- Subjects: ➤ Force distribution - Lift - Loads (Forces) - Rolling moments - Subsonic speed - Vortex lattice method - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17594006M - OL15507839M - OL17126890M - OL18122121M
- Online Computer Library Center (OCLC) ID: 40348464
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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4Key topics for high-lift research
By David Fisher
“Key topics for high-lift research” Metadata:
- Title: ➤ Key topics for high-lift research
- Author: David Fisher
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Key topics for high-lift research” Subjects and Themes:
- Subjects: ➤ F-15 aircraft - Aerodynamics - Fins - Flow distribution - Lift - Airfoils - Wind tunnel tests - Flight tests
Edition Identifiers:
- The Open Library ID: OL17565560M - OL15492341M - OL17124491M - OL18116300M
- Online Computer Library Center (OCLC) ID: 39517789
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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5The effects of crossflow on the pressures and lift induced by the fountain generated between two impinging jets
By Richard E. Kuhn
“The effects of crossflow on the pressures and lift induced by the fountain generated between two impinging jets” Metadata:
- Title: ➤ The effects of crossflow on the pressures and lift induced by the fountain generated between two impinging jets
- Author: Richard E. Kuhn
- Language: English
- Number of Pages: Median: 60
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - Ames Research Center - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Moffett Field, Calif - [Washington, D.C.] - [Springfield, Va
“The effects of crossflow on the pressures and lift induced by the fountain generated between two impinging jets” Subjects and Themes:
- Subjects: ➤ Aerodynamics - Cross flow - Ground-cushion phenomenon - Lift - STOVL aircraft - Vertically rising aircraft - Vortex-motion
Edition Identifiers:
- The Open Library ID: OL15543273M - OL17597305M - OL19425818M
- Online Computer Library Center (OCLC) ID: 41363691
Author's Alternative Names:
"R. E. Kuhn"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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6In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)
By Edwin J. Saltzman
“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Metadata:
- Title: ➤ In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)
- Author: Edwin J. Saltzman
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program - National Technical Information Service, distributor]
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisions with contemporary aircraft)” Subjects and Themes:
- Subjects: ➤ X-29 aircraft - Wave drag - Lift - Airfoil profiles - Swept forward wings - Drag - Transonic speed
Edition Identifiers:
- The Open Library ID: OL18080007M - OL17008295M - OL15411782M
- Online Computer Library Center (OCLC) ID: 32938383
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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7Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations
By Gregory M. Gatlin
“Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations” Metadata:
- Title: ➤ Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations
- Author: Gregory M. Gatlin
- Language: English
- Number of Pages: Median: 43
- 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: 1989
- Publish Location: ➤ Hampton, Va - [Springfield, Va - [Washington, D.C.]
“Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerospace planes - Body-wing configurations - Hypersonic flow - Hypersonic planes - Lift (Aerodynamics) - Lift - Aircraft design
Edition Identifiers:
- The Open Library ID: OL19380187M - OL18263011M - OL16137788M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
By Gregory M. Catlin
“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” Metadata:
- Title: ➤ Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes
- Author: Gregory M. Catlin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Low-speed longitudinal aerodynamic characteristics through poststall for twenty-one novel planform shapes” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Flow visualization - Forebodies - Highly maneuverable aircraft - Lift - Low aspect ratio wings - Low speed - Pitching moments - Swept wings - Wind tunnel tests - Wing planforms
Edition Identifiers:
- The Open Library ID: OL17041056M - OL15426200M - OL18088687M
- Online Computer Library Center (OCLC) ID: 35587781
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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9Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions
By Farhad Ghaffari
“Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions” Metadata:
- Title: ➤ Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions
- Author: Farhad Ghaffari
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 2002
- Publish Location: Hampton, VA - [Springfield, Va
“Turbulent Navier-Stokes flow analysis of an advanced semispan diamond-wing model in tunnel and free air at high-lift conditions” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Low aspect ratio wings - Semispan models - Turbulent flow - Wind tunnel tests - Navier-Stokes equation - Lift - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL17725170M - OL18227514M - OL19146725M
Access and General Info:
- First Year Published: 2002
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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10High-lift flight tunnel
By David Lofftus
“High-lift flight tunnel” Metadata:
- Title: High-lift flight tunnel
- Author: David Lofftus
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2000
- Publish Location: Hanover, MD - Hampton, Va
“High-lift flight tunnel” Subjects and Themes:
- Subjects: ➤ Flight tests - Ground tests - High Reynolds number - Lift - Mach number - Test facilities - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17607425M - OL18171258M - OL16030609M
- Online Computer Library Center (OCLC) ID: 50152830
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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11A first scramjet study
By George Emmanuel
“A first scramjet study” Metadata:
- Title: A first scramjet study
- Author: George Emmanuel
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1989
- Publish Location: ➤ [Washington, DC - Springfield, Va
“A first scramjet study” Subjects and Themes:
- Subjects: ➤ Temperature effects - Lift - Nozzle flow - Thrust - Hypersonic speed - Supersonic combustion ramjet engines
Edition Identifiers:
- The Open Library ID: OL14972502M - OL17683624M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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12Multi-element airfoil optimization for maximum lift at high Reynolds numbers
By Walter O. Valarezo
“Multi-element airfoil optimization for maximum lift at high Reynolds numbers” Metadata:
- Title: ➤ Multi-element airfoil optimization for maximum lift at high Reynolds numbers
- Author: Walter O. Valarezo
- Language: English
- Number of Pages: Median: 976
- Publisher: ➤ American Institute of Aeronautics and Astronautics
- Publish Date: 1991
- Publish Location: New York
“Multi-element airfoil optimization for maximum lift at high Reynolds numbers” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19243245M - OL20379435M
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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13Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
By Jensen Lin
“Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation” Metadata:
- Title: ➤ Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation
- Author: Jensen Lin
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Dryden Flight Research Center - National Technical Information Service, distributor
- Publish Date: 2000
- Publish Location: ➤ Edwards, Calif - [Springfield, Va
“Aerodynamic lift and moment calculations using a closed-form solution of the Possio equation” Subjects and Themes:
- Subjects: ➤ Aerodynamic coefficients - Aeroelasticity - Laplace transformation - Lift - Method of moments - Unsteady aerodynamics
Edition Identifiers:
- The Open Library ID: OL17596830M - OL17704161M
- Online Computer Library Center (OCLC) ID: 45009645
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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14A 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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15Description of panel method code ANTARES
By Norbert Ulbrich
“Description of panel method code ANTARES” Metadata:
- Title: ➤ Description of panel method code ANTARES
- Author: Norbert Ulbrich
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2000
- Publish Location: ➤ Moffett, Field, Calif - Hanover, MD
“Description of panel method code ANTARES” Subjects and Themes:
- Subjects: ➤ Aerodynamic interference - Computer programs - Lift - Rectangular wind tunnels - Subsonic flow - Wall flow - Wind tunnel models - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL16030491M - OL17607419M
- Online Computer Library Center (OCLC) ID: 50075150
Access and General Info:
- First Year Published: 2000
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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16Mechanical design of high lift systems for high aspect ratio swept wings
By Peter K. C. Rudolph
“Mechanical design of high lift systems for high aspect ratio swept wings” Metadata:
- Title: ➤ Mechanical design of high lift systems for high aspect ratio swept wings
- Author: Peter K. C. Rudolph
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Mechanical design of high lift systems for high aspect ratio swept wings” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Angle of attack - Boeing 757 aircraft - Design analysis - European Airbus - Lift
Edition Identifiers:
- The Open Library ID: OL15548655M - OL17595589M
- Online Computer Library Center (OCLC) ID: 41969370
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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17Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing
By Dhanvada M. Rao
“Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing” Metadata:
- Title: ➤ Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing
- Author: Dhanvada M. Rao
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va - [Springfield, Va
“Low-speed wind tunnel study of longitudinal stability and usable-lift improvement of a cranked wing” Subjects and Themes:
- Subjects: Longitudinal stability - Wind tunnel tests - Lift - Swept wings - Vortices
Edition Identifiers:
- The Open Library ID: OL18083221M - OL17684515M
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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18Study 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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19Measurements of shear lift force on a bubble in channel flow in microgravity
By Henry K. Nahra
“Measurements of shear lift force on a bubble in channel flow in microgravity” Metadata:
- Title: ➤ Measurements of shear lift force on a bubble in channel flow in microgravity
- Author: Henry K. Nahra
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Glenn Research Center - Available from NASA Center for Aerospace Information
- Publish Date: 2003
- Publish Location: ➤ [Cleveland, Ohio] - Hanover, MD
“Measurements of shear lift force on a bubble in channel flow in microgravity” Subjects and Themes:
- Subjects: ➤ Bubbles - Channel flow - Drops (Liquids) - Lift - Microgravity - Numerical analysis
Edition Identifiers:
- The Open Library ID: OL17621425M - OL17723980M
- Online Computer Library Center (OCLC) ID: 55975584
Access and General Info:
- First Year Published: 2003
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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20A 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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21Noise impact of advanced high lift systems
By Kevin R. Elmer
“Noise impact of advanced high lift systems” Metadata:
- Title: ➤ Noise impact of advanced high lift systems
- Author: Kevin R. Elmer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Noise impact of advanced high lift systems” Subjects and Themes:
- Subjects: ➤ Aeroacoustics - Aerodynamic noise - Aircraft design - Engine noise - Jet aircraft noise - Lift - Noise reduction - Passenger aircraft - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL15416073M - OL17791319M
- Online Computer Library Center (OCLC) ID: 33241385
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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22The Helicopter
History, Piloting, and How It Flies
By John Foster Fay
“The Helicopter” Metadata:
- Title: The Helicopter
- Author: John Foster Fay
- Language: English
- Number of Pages: Median: 194
- Publisher: David & Charles
- Publish Date: 1976
- Publish Location: ➤ Newton Abbot - North Pomfret, Vt
“The Helicopter” Subjects and Themes:
- Subjects: ➤ aeronautics - flight - Helicopters - aerodynamics - lift - helicopter - piloting
- People: Igor Sikorsky - Juan de la Cierva
Edition Identifiers:
- The Open Library ID: OL4598052M
- Library of Congress Control Number (LCCN): 77360773
- All ISBNs: 0715372491 - 9780715372494
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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23Modeling of longitudinal unsteady aerodynamics of a wing-tail combination
By Vladislav Klein
“Modeling of longitudinal unsteady aerodynamics of a wing-tail combination” Metadata:
- Title: ➤ Modeling of longitudinal unsteady aerodynamics of a wing-tail combination
- Author: Vladislav Klein
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Modeling of longitudinal unsteady aerodynamics of a wing-tail combination” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic stability - Lift - Longitudinal stability - Pitching moments - Uunsteady aerodynamics - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15559425M
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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24An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet
By Richard E. Kuhn
“An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet” Metadata:
- Title: ➤ An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet
- Author: Richard E. Kuhn
- 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
“An analysis of the pressures, forces and moments induced by the ground vortex generated by a single impinging jet” Subjects and Themes:
- Subjects: ➤ Ground effect (Aerodynamics) - Lift - Pitching moments - Pressure distribution - STOVL aircraft - Vortices - Wall jets
Edition Identifiers:
- The Open Library ID: OL15504968M
Author's Alternative Names:
"R. E. Kuhn"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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25Piloted simulation study of the effect of high-lift aerodynamics on the takeoff noise of a representative high-speed civil transport
By Louis J. Glaab
“Piloted simulation study of the effect of high-lift aerodynamics on the takeoff noise of a representative high-speed civil transport” Metadata:
- Title: ➤ Piloted simulation study of the effect of high-lift aerodynamics on the takeoff noise of a representative high-speed civil transport
- Author: Louis J. Glaab
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: [Springfield, Va - Hampton, Va
“Piloted simulation study of the effect of high-lift aerodynamics on the takeoff noise of a representative high-speed civil transport” Subjects and Themes:
- Subjects: ➤ Pilot support systems - Computerized simulation - Takeoff - Noise intensity - Aerodynamic noise - Aircraft configurations - Noise prediction (Aircraft) - Noise reduction - Lift
Edition Identifiers:
- The Open Library ID: OL15569357M
- Online Computer Library Center (OCLC) ID: 44447728
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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26Effect of in-flight ice accretion on the performance of a multi-element airfoil
By Abdollah Khodadoust
“Effect of in-flight ice accretion on the performance of a multi-element airfoil” Metadata:
- Title: ➤ Effect of in-flight ice accretion on the performance of a multi-element airfoil
- Author: Abdollah Khodadoust
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Effect of in-flight ice accretion on the performance of a multi-element airfoil” Subjects and Themes:
- Subjects: ➤ Reynolds number - Lift - Airfoils - Aircraft icing - Wind tunnel tests - Angle of attack
Edition Identifiers:
- The Open Library ID: OL17837129M
- Online Computer Library Center (OCLC) ID: 39777276
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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27In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft)
By Edwin J. Saltzman
“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft)” Metadata:
- Title: ➤ In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft)
- Author: Edwin J. Saltzman
- Number of Pages: Median: 57
- Publisher: ➤ Dryden Flight Research Facility
- Publish Date: 1994
- Publish Location: Edwards, Calif
“In-flight lift-drag characteristics for a forward-swept wing aircraft (and comparisons with contemporary aircraft)” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19006158M
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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28Moving base simulation of an ASTOVL Lift-fan aircraft
By William W. Y. Chung
“Moving base simulation of an ASTOVL Lift-fan aircraft” Metadata:
- Title: ➤ Moving base simulation of an ASTOVL Lift-fan aircraft
- Author: William W. Y. Chung
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Moving base simulation of an ASTOVL Lift-fan aircraft” Subjects and Themes:
- Subjects: ➤ Dynamic response - Aircraft control - STOVL aircraft - Propulsion system performance - Flight characteristics - Lift - Engine control - Lift fans - Fighter aircraft - Man machine systems - Computerized simulation
Edition Identifiers:
- The Open Library ID: OL15421553M
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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29Noise exposure reduction of advanced high-lift systems
By Stephen W. Haffner
“Noise exposure reduction of advanced high-lift systems” Metadata:
- Title: ➤ Noise exposure reduction of advanced high-lift systems
- Author: Stephen W. Haffner
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: [Springfield, Va - Hampton, Va
“Noise exposure reduction of advanced high-lift systems” Subjects and Themes:
- Subjects: ➤ Aircraft noise - Lift - Aeroacoustics - Aerodynamic noise - Noise reduction - Lift drag ratio - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL15413660M
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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30Survey and analysis of research on supersonic drag-due-to-lift minimization with recommendations for wing design
By Harry W. Carlson
“Survey and analysis of research on supersonic drag-due-to-lift minimization with recommendations for wing design” Metadata:
- Title: ➤ Survey and analysis of research on supersonic drag-due-to-lift minimization with recommendations for wing design
- Author: Harry W. Carlson
- Number of Pages: Median: 153
- Publisher: Langley Research Center
- Publish Date: 1992
- Publish Location: Hampton, Va
“Survey and analysis of research on supersonic drag-due-to-lift minimization with recommendations for wing design” Subjects and Themes:
- Subjects: Lift - Supersonic drag - Wings
Edition Identifiers:
- The Open Library ID: OL19246143M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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31A simplified method for estimating subsonic lift-curve slope at low angles of attack for irregular planform wings
By Bernard Spencer
“A simplified method for estimating subsonic lift-curve slope at low angles of attack for irregular planform wings” Metadata:
- Title: ➤ A simplified method for estimating subsonic lift-curve slope at low angles of attack for irregular planform wings
- Author: Bernard Spencer
- Number of Pages: Median: 31
- Publisher: Langley Research Center
- Publish Date: 1961
- Publish Location: Langley Field, Va
“A simplified method for estimating subsonic lift-curve slope at low angles of attack for irregular planform wings” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL20984881M
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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32Lift and drag of a wing spanning a free jet
By H. Glauert
“Lift and drag of a wing spanning a free jet” Metadata:
- Title: ➤ Lift and drag of a wing spanning a free jet
- Author: H. Glauert
- Publisher: HMSO
- Publish Date: 1934
- Publish Location: London
“Lift and drag of a wing spanning a free jet” Subjects and Themes:
Edition Identifiers:
- The Open Library ID: OL19247245M
Access and General Info:
- First Year Published: 1934
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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33Annual progress report ... entitled An experimental investigation of the flow physics of high-lift systems, for the period March-December 1995
By Flint O. Thomas
“Annual progress report ... entitled An experimental investigation of the flow physics of high-lift systems, for the period March-December 1995” Metadata:
- Title: ➤ Annual progress report ... entitled An experimental investigation of the flow physics of high-lift systems, for the period March-December 1995
- Author: Flint O. Thomas
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Annual progress report ... entitled An experimental investigation of the flow physics of high-lift systems, for the period March-December 1995” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Lift - Airfoil profiles - Flow visualization - Aircraft design - Boundary layer flow - Laminar flow
Edition Identifiers:
- The Open Library ID: OL15424660M
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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34Neural 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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35An 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
Online Access
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36On the lift and induced drag associated with large downwash angles
By Herbert S. Ribner
“On the lift and induced drag associated with large downwash angles” Metadata:
- Title: ➤ On the lift and induced drag associated with large downwash angles
- Author: Herbert S. Ribner
- Number of Pages: Median: 15
- Publisher: Institute of Aerophysics
- Publish Date: 1958
- Publish Location: [Downsview, Ont.]
“On the lift and induced drag associated with large downwash angles” Subjects and Themes:
- Subjects: Downwash - Drag - Lift - Short takeoff aircraft
Edition Identifiers:
- The Open Library ID: OL19004025M
Access and General Info:
- First Year Published: 1958
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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37Computation of lifting wing-flap configurations
By Brian Cantwell
“Computation of lifting wing-flap configurations” Metadata:
- Title: ➤ Computation of lifting wing-flap configurations
- Author: Brian Cantwell
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Computation of lifting wing-flap configurations” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Computational grids - Pressure distribution - Turbulence models - Flow distribution - Lift - Aerodynamic configurations - Wing flaps
Edition Identifiers:
- The Open Library ID: OL15507284M
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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38Study of the TRAC airfoil table computational system
By Hong Hu
“Study of the TRAC airfoil table computational system” Metadata:
- Title: ➤ Study of the TRAC airfoil table computational system
- Author: Hong Hu
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Study of the TRAC airfoil table computational system” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Aerodynamic coefficients - Navier-Stokes equation - Pitching moments - Drag - Lift - Airfoils - Noise reduction - Computer programs - Aerodynamic noise
Edition Identifiers:
- The Open Library ID: OL15550693M
Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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39Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise
By Donald B. Hanson
“Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise” Metadata:
- Title: ➤ Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise
- Author: Donald B. Hanson
- Number of Pages: Median: 130
- Publisher: Lewis Research Center
- Publish Date: 1991
- Publish Location: Cleveland, Ohio
“Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. Volume 1 - Development of theory for blade loading, wakes and noise” Subjects and Themes:
- Subjects: Turboprop engines - Lift - Wakes - Blades
Edition Identifiers:
- The Open Library ID: OL19165524M
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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40Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory
By E. Carson Yates
“Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory” Metadata:
- Title: ➤ Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory
- Author: E. Carson Yates
- Language: English
- Number of Pages: Median: 16
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va - [Springfield, Va
“Aerodynamic sensitivities from subsonic, sonic, and supersonic unsteady, nonplanar lifting-surface theory” Subjects and Themes:
- Subjects: ➤ Surfaces - Lift - Aerodynamic coefficients - Unsteady flow - Aerodynamics - Sensitivity - Subsonic speed
Edition Identifiers:
- The Open Library ID: OL15409051M
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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41Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction
By Stephen E. Dunagan
“Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction” Metadata:
- Title: ➤ Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction
- Author: Stephen E. Dunagan
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - For sale by the National Technical Information Service
- Publish Date: 1987
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Lift distribution and velocity field measurements for a three-dimensional, steady blade/vortex interaction” Subjects and Themes:
- Subjects: ➤ Velocity distribution - Helicopters - Blade-vortex interaction - Lift - Force distribution - Rotors
Edition Identifiers:
- The Open Library ID: OL15410983M
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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42A 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
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43Moving base simulation of an ASTOVL Lift-fan aircraft
By William Chung
“Moving base simulation of an ASTOVL Lift-fan aircraft” Metadata:
- Title: ➤ Moving base simulation of an ASTOVL Lift-fan aircraft
- Author: William Chung
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Moving base simulation of an ASTOVL Lift-fan aircraft” Subjects and Themes:
- Subjects: ➤ Dynamic response - Aircraft control - STOVL aircraft - Propulsion system performance - Flight characteristics - Lift - Engine control - Lift fans - Fighter aircraft - Man machine systems - Computerized simulation
Edition Identifiers:
- The Open Library ID: OL17117405M
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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44A wind tunnel investigation of the effects of micro-vortex generators and Gurney flaps on the high-lift characteristics of a business jet wing
By Michelle Therese Martuccio
“A wind tunnel investigation of the effects of micro-vortex generators and Gurney flaps on the high-lift characteristics of a business jet wing” Metadata:
- Title: ➤ A wind tunnel investigation of the effects of micro-vortex generators and Gurney flaps on the high-lift characteristics of a business jet wing
- Author: Michelle Therese Martuccio
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC - Springfield, Va
“A wind tunnel investigation of the effects of micro-vortex generators and Gurney flaps on the high-lift characteristics of a business jet wing” Subjects and Themes:
- Subjects: ➤ Wing flaps - Lift - Vortices - Lift devices - Vortex generators - Jet flaps - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15414556M
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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Find A wind tunnel investigation of the effects of micro-vortex generators and Gurney flaps on the high-lift characteristics of a business jet wing at online marketplaces:
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45Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
By Steven M. Klausmeyer
“Comparative results from a CFD challenge over a 2D three-element high-lift airfoil” Metadata:
- Title: ➤ Comparative results from a CFD challenge over a 2D three-element high-lift airfoil
- Author: Steven M. Klausmeyer
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: [Springfield, Va - Hampton, Va
“Comparative results from a CFD challenge over a 2D three-element high-lift airfoil” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Aerodynamic coefficients - Lift - Airfoils - Navier-Stokes equation - Aerodynamic characteristics
Edition Identifiers:
- The Open Library ID: OL15497745M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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46An approach to the constrained design of natural laminar flow airfoils
By Bradford Earl Green
“An approach to the constrained design of natural laminar flow airfoils” Metadata:
- Title: ➤ An approach to the constrained design of natural laminar flow airfoils
- Author: Bradford Earl Green
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, D.C - Springfield, Va
“An approach to the constrained design of natural laminar flow airfoils” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Turbulent boundary layer - Lift - Aerodynamic coefficients - Laminar flow airfoils - Laminar boundary layer - Pressure distribution
Edition Identifiers:
- The Open Library ID: OL15498378M
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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47Numerical design of advanced multi-element airfoils
By Donovan L. Mathias
“Numerical design of advanced multi-element airfoils” Metadata:
- Title: ➤ Numerical design of advanced multi-element airfoils
- Author: Donovan L. Mathias
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration - California Polytechnic State University
- Publish Date: 1994
- Publish Location: ➤ San Luis Obispo, CA - Springfield, Va - [Washington, DC
“Numerical design of advanced multi-element airfoils” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Lift - Transport aircraft - Unswept wings - Three dimensional flow - Wing flaps
Edition Identifiers:
- The Open Library ID: OL15410087M
Access and General Info:
- First Year Published: 1994
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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48Unsteady potential flow past a propeller blade section
By Mohammad Ali Takallu
“Unsteady potential flow past a propeller blade section” Metadata:
- Title: ➤ Unsteady potential flow past a propeller blade section
- Author: Mohammad Ali Takallu
- Language: English
- Number of Pages: Median: 25
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1990
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“Unsteady potential flow past a propeller blade section” Subjects and Themes:
- Subjects: ➤ Aerial Propellers - Flow distribution - Lift - Potential flow - Pressure distribution - Propeller blades - Propellers, Aerial - Unsteady flow - Unsteady flow (Aerodynamics)
Edition Identifiers:
- The Open Library ID: OL16131163M
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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49Oscillating behaviour of a 7.5% circular arc airfoil
By David James Ahier
“Oscillating behaviour of a 7.5% circular arc airfoil” Metadata:
- Title: ➤ Oscillating behaviour of a 7.5% circular arc airfoil
- Author: David James Ahier
- Publisher: ➤ Dept. of Aerospace Science and Engineering
- Publish Date: 1987
- Publish Location: [Downsview, Ont.]
“Oscillating behaviour of a 7.5% circular arc airfoil” Subjects and Themes:
- Subjects: Oscillating wing aerodynamics - Lift
Edition Identifiers:
- The Open Library ID: OL19000044M
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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50Experiments on the lift and drag of spheres suspended in a Poiseuille flow
By R. Eichhorn
“Experiments on the lift and drag of spheres suspended in a Poiseuille flow” Metadata:
- Title: ➤ Experiments on the lift and drag of spheres suspended in a Poiseuille flow
- Author: R. Eichhorn
- Number of Pages: Median: 32
- Publisher: ➤ Dept. of Aerospace Engineering, School of Engineering and Applied Science, University of Virginia
- Publish Date: 1964
- Publish Location: Charlottesville, Va
“Experiments on the lift and drag of spheres suspended in a Poiseuille flow” Subjects and Themes:
- Subjects: Spheres - Drag - Lift - Laminar flow
Edition Identifiers:
- The Open Library ID: OL19003333M
Access and General Info:
- First Year Published: 1964
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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