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Source: The Open Library
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1Numerical solutions of the complete Navier-Stokes equations
By H. A. Hassan
“Numerical solutions of the complete Navier-Stokes equations” Metadata:
- Title: ➤ Numerical solutions of the complete Navier-Stokes equations
- Author: H. A. Hassan
- Language: English
- Publisher: ➤ Dept. of Mechanical and Aerospace Engineering, North Carolina State University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1989 - 1994 - 1995 - 1996
- Publish Location: ➤ Raleigh, N.C - [Washington, DC - Springfield, Va - [Washington, D.C
“Numerical solutions of the complete Navier-Stokes equations” Subjects and Themes:
- Subjects: ➤ Navier-Stokes equation - Turbulent flow - Turbulence models - Eddy viscosity - Flow velocity - Supersonic combustion - Mixing layers (Fluids) - Jet flow - Navier-Stokes equations - Compressible flow - Compressibility - Numerical solutions - Turbulent mixing - Computational fluid dynamics - Numerical analysis - Vorticity - Boundary layer separation - Vortices - Pressure gradients - Three dimensional flow - Aerodynamic characteristics - Airfoils
Edition Identifiers:
- The Open Library ID: OL15452379M - OL16135487M - OL15419184M - OL14706079M
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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2Swept-wing receptivity studies using distributed roughness
By W. S. Saric
“Swept-wing receptivity studies using distributed roughness” Metadata:
- Title: ➤ Swept-wing receptivity studies using distributed roughness
- Author: W. S. Saric
- Language: English
- Publisher: ➤ Mechanical and Aerospace Engineering, College of Engineering and Applied Science, Arizona State University - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Tempe, AZ - [Springfield, Va - Hampton, Va
“Swept-wing receptivity studies using distributed roughness” Subjects and Themes:
- Subjects: Pressure gradients - Cross flow - Swept wings - Nonlinearity - Boundary layer transition
Edition Identifiers:
- The Open Library ID: OL17583482M - OL17132992M - OL18134575M - OL15547477M
- Online Computer Library Center (OCLC) ID: 41993468
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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3Improved two-equation k - [omega] turbulence models for aerodynamic flows
By Florian R. Menter
“Improved two-equation k - [omega] turbulence models for aerodynamic flows” Metadata:
- Title: ➤ Improved two-equation k - [omega] turbulence models for aerodynamic flows
- Author: Florian R. Menter
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1992
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Improved two-equation k - [omega] turbulence models for aerodynamic flows” Subjects and Themes:
- Subjects: ➤ Boundary layers - Flow distribution - Free flow - Pressure gradients - Shear layers - Shear stress - Turbulence models - Turbulent flow
Edition Identifiers:
- The Open Library ID: OL15404624M - OL18076669M - OL17114103M - OL17009627M
- Online Computer Library Center (OCLC) ID: 32333258
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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4A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel
By Stephen P. Wilkinson
“A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel” Metadata:
- Title: ➤ A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel
- Author: Stephen P. Wilkinson
- Language: English
- Publisher: ➤ American Institute of Astronautics and Aeronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ Reston, VA - Springfield, Va - [Washington, D.C
“A review of hypersonic boundary layer stability experiments in a quiet Mach 6 wind tunnel” Subjects and Themes:
- Subjects: ➤ Pressure gradients - Cooling - Boundary layer stability - Hypersonic boundary layer - Additives - Angle of attack
Edition Identifiers:
- The Open Library ID: OL15503895M - OL18121122M - OL17838510M
- Online Computer Library Center (OCLC) ID: 40426210
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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5Higher-order approximations in interactive airfoil calculations
By D. W. Zingg
“Higher-order approximations in interactive airfoil calculations” Metadata:
- Title: ➤ Higher-order approximations in interactive airfoil calculations
- Author: D. W. Zingg
- Language: English
- Number of Pages: Median: 102
- Publisher: ➤ University of Toronto - Institute for Aerospace Studies
- Publish Date: 1987 - 1988
- Publish Location: [Downsview, Ont.]
“Higher-order approximations in interactive airfoil calculations” Subjects and Themes:
- Subjects: ➤ Airfoils - Boundary layers - Computational fluid dynamics - Incompressible flow - Interactive methods - Pressure gradients - Subsonic flow
Edition Identifiers:
- The Open Library ID: OL19987220M - OL20898250M - OL20697434M
Author's Alternative Names:
"David W. Zingg"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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6Flow characteristics in boundary layer bleed slots with plenum
By A. Hamed
“Flow characteristics in boundary layer bleed slots with plenum” Metadata:
- Title: ➤ Flow characteristics in boundary layer bleed slots with plenum
- Author: A. Hamed
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - For sale by the National Technical Information Service
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, D.C
“Flow characteristics in boundary layer bleed slots with plenum” Subjects and Themes:
- Subjects: ➤ Boundary layer control - Boundary layer flow - Flow characteristics - Oblique shock waves - Plenum chambers - Pressure gradients - Shock wave interaction - Slots - Supersonic flow - Turbulent boundary layer
Edition Identifiers:
- The Open Library ID: OL15419025M - OL17793989M
- Online Computer Library Center (OCLC) ID: 34757915
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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7Wake measurements in a strong adverse pressure gradient
By R. Hoffenberg
“Wake measurements in a strong adverse pressure gradient” Metadata:
- Title: ➤ Wake measurements in a strong adverse pressure gradient
- Author: R. Hoffenberg
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Wake measurements in a strong adverse pressure gradient” Subjects and Themes:
- Subjects: ➤ Flow distribution - Lift devices - Pressure effects - Pressure gradients - Wakes - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL17788542M - OL15411517M
- Online Computer Library Center (OCLC) ID: 32909494
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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8Nonlinear stability of oscillatory core-annular flow
By Adrian V. Coward
“Nonlinear stability of oscillatory core-annular flow” Metadata:
- Title: ➤ Nonlinear stability of oscillatory core-annular flow
- Author: Adrian V. Coward
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, VA
“Nonlinear stability of oscillatory core-annular flow” Subjects and Themes:
- Subjects: ➤ Asymptotic series - Compressible flow - Flow stability - Fluid dynamics - Harmonic oscillation - Interfacial tension - Navier-Stokes equation - Nonlinearity - Periodic functions - Pressure effects - Pressure gradients - Two phase flow - Viscosity - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17790342M - OL15404320M
- Online Computer Library Center (OCLC) ID: 32298644
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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9A root-mean-square pressure fluctuations model for internal flow applications
By Y. S. Chen
“A root-mean-square pressure fluctuations model for internal flow applications” Metadata:
- Title: ➤ A root-mean-square pressure fluctuations model for internal flow applications
- Author: Y. S. Chen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Branch - For sale by the National Technical Information Service]
- Publish Date: 1985
- Publish Location: ➤ [Washington, DC] - [Springfield, Va
“A root-mean-square pressure fluctuations model for internal flow applications” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Internal flow - Pressure gradients - Turbulence - Root-mean-square errors - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL18082562M - OL15416026M
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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10Experimental and theoretical studies of capillary-pumped loop heat pipes
By N. T. Obot
“Experimental and theoretical studies of capillary-pumped loop heat pipes” Metadata:
- Title: ➤ Experimental and theoretical studies of capillary-pumped loop heat pipes
- Author: N. T. Obot
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Clarkson University - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Potsdam, N.Y - Springfield, Va - [Washington, D.C
“Experimental and theoretical studies of capillary-pumped loop heat pipes” Subjects and Themes:
- Subjects: Pressure gradients - Capillary flow - Heat transfer - Heat pipes - Computerized simulation
Edition Identifiers:
- The Open Library ID: OL17679546M - OL17792264M
- Online Computer Library Center (OCLC) ID: 34765938
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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11On the prediction of free turbulent jets with swirl using a quadratic pressure-strain model
By Bassam A. Younis
“On the prediction of free turbulent jets with swirl using a quadratic pressure-strain model” Metadata:
- Title: ➤ On the prediction of free turbulent jets with swirl using a quadratic pressure-strain model
- Author: Bassam A. Younis
- Language: English
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center, Institute for Computer Applications in Science and Engineering
- Publish Date: 1994
- Publish Location: Hampton, Va - [Springfield, Va
“On the prediction of free turbulent jets with swirl using a quadratic pressure-strain model” Subjects and Themes:
- Subjects: ➤ Free jets - Jet flow - Predictions - Pressure gradients - Reynolds stress - Shear stress - Stress tensors - Swirling - Turbulent jets
Edition Identifiers:
- The Open Library ID: OL15408457M - OL17790645M
- Online Computer Library Center (OCLC) ID: 32660420
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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12A modified mixing length turbulence model for zero and adverse pressure gradients
By J. M. Conley and B. P. Leonard
“A modified mixing length turbulence model for zero and adverse pressure gradients” Metadata:
- Title: ➤ A modified mixing length turbulence model for zero and adverse pressure gradients
- Authors: J. M. ConleyB. P. Leonard
- Language: English
- Publisher: ➤ [National Technical Information Service, distributor] - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Washington, DC] - [Springfield, VA] - [Springfield, Va
“A modified mixing length turbulence model for zero and adverse pressure gradients” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Turbulent flow - Turbulent boundary layer - Mixing length flow theory - Pressure gradients - Turbulence models
Edition Identifiers:
- The Open Library ID: OL18078587M - OL15408463M
- Online Computer Library Center (OCLC) ID: 32660592
Author's Alternative Names:
"J.M Conley"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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13The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients
By Jon A. Hoffmann
“The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients” Metadata:
- Title: ➤ The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients
- Author: Jon A. Hoffmann
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Aeronautical Engineering Dept., California Polytechnic State University ; [Washington, D.C. - National Technical Information Service, distributor
- Publish Date: 1988
- Publish Location: ➤ Springfield, Va - San Luis Obispo, Calif
“The influence of free-stream turbulence on turbulent boundary layers with mild adverse pressure gradients” Subjects and Themes:
- Subjects: Pressure gradients - Turbulent boundary layer - Free flow - Isotropic turbulence
Edition Identifiers:
- The Open Library ID: OL15409954M - OL18079291M
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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14The effect of crossflow on Görtler vortices
By S. R. Otto
“The effect of crossflow on Görtler vortices” Metadata:
- Title: ➤ The effect of crossflow on Görtler vortices
- Author: S. R. Otto
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Institute for Computer Applications in Science and Engineering, NASA Langley Research Center
- Publish Date: 1994
- Publish Location: Hampton, VA - [Springfield, Va
“The effect of crossflow on Görtler vortices” Subjects and Themes:
- Subjects: Boundary layer flow - Cross flow - Goertler instability - Pressure gradients - Vortices
Edition Identifiers:
- The Open Library ID: OL15381538M
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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15The thin oil film equation
By Brown, James L.
“The thin oil film equation” Metadata:
- Title: The thin oil film equation
- Author: Brown, James L.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“The thin oil film equation” Subjects and Themes:
- Subjects: ➤ Burger equation - Gravitation - Partial Differential equations - Pressure gradients - Thin films - Three dimensional flow
Edition Identifiers:
- The Open Library ID: OL15552315M
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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16The influence of high adverse pressure gradients on boundary layers in supersonic flow
By John D. Lee
“The influence of high adverse pressure gradients on boundary layers in supersonic flow” Metadata:
- Title: ➤ The influence of high adverse pressure gradients on boundary layers in supersonic flow
- Author: John D. Lee
- Number of Pages: Median: 29
- Publisher: Institute of Aerophysics
- Publish Date: 1952
- Publish Location: [Downsview, Ont.]
“The influence of high adverse pressure gradients on boundary layers in supersonic flow” Subjects and Themes:
- Subjects: Boundary layers - Pressure gradients - Supersonic flow
Edition Identifiers:
- The Open Library ID: OL20897524M
Access and General Info:
- First Year Published: 1952
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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17Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers
By Meelan Choudhari
“Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers” Metadata:
- Title: ➤ Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers
- Author: Meelan Choudhari
- 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
“Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers” Subjects and Themes:
- Subjects: ➤ Laminar boundary layer - Sound waves - Reynolds number - Pressure gradients - Falkner-Skan equation - Transition flow - Boundary-layer transition
Edition Identifiers:
- The Open Library ID: OL15410434M
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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18Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer
By Abdelkader Frendi
“Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer” Metadata:
- Title: ➤ Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer
- Author: Abdelkader Frendi
- 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
“Effect of pressure gradients on plate response and radiation in a supersonic turbulent boundary layer” Subjects and Themes:
- Subjects: Pressure gradients - Supersonic boundary layers - Turbulent boundary layer - High frequencies - Boundary layer thickness
Edition Identifiers:
- The Open Library ID: OL15505121M
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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19Modification of a variational objective analysis model for new equations for pressure gradient and vertical velocity in the lower troposphere and for spatial resolution and accuracy of satellite data
By Gary L. Achtemeier
“Modification of a variational objective analysis model for new equations for pressure gradient and vertical velocity in the lower troposphere and for spatial resolution and accuracy of satellite data” Metadata:
- Title: ➤ Modification of a variational objective analysis model for new equations for pressure gradient and vertical velocity in the lower troposphere and for spatial resolution and accuracy of satellite data
- Author: Gary L. Achtemeier
- Language: English
- Number of Pages: Median: 26
- 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
“Modification of a variational objective analysis model for new equations for pressure gradient and vertical velocity in the lower troposphere and for spatial resolution and accuracy of satellite data” Subjects and Themes:
- Subjects: ➤ Mathematical models - Troposphere - Atmospheric circulation - Variance (Statistics) - Satellite meteorology - Pressure gradients - Meteorological satellites - Winds aloft
Edition Identifiers:
- The Open Library ID: OL15417263M
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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20Summary of work on shock wave feature extraction in 3-D datasets
By Lambertus Hesselink
“Summary of work on shock wave feature extraction in 3-D datasets” Metadata:
- Title: ➤ Summary of work on shock wave feature extraction in 3-D datasets
- Author: Lambertus Hesselink
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC
“Summary of work on shock wave feature extraction in 3-D datasets” Subjects and Themes:
- Subjects: ➤ Perturbation - Numerical flow visualization - Pressure gradients - Three dimensional flow - Mach number - Shock waves
Edition Identifiers:
- The Open Library ID: OL15506359M
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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21Experimental Reynolds analogy factor for a compressible turbulent boundary layer with a pressure gradient
By Lionel Pasiuk
“Experimental Reynolds analogy factor for a compressible turbulent boundary layer with a pressure gradient” Metadata:
- Title: ➤ Experimental Reynolds analogy factor for a compressible turbulent boundary layer with a pressure gradient
- Author: Lionel Pasiuk
- Publisher: U.S. Naval Ordnance Laboratory
- Publish Date: 1964
- Publish Location: White Oak, Md
“Experimental Reynolds analogy factor for a compressible turbulent boundary layer with a pressure gradient” Subjects and Themes:
- Subjects: Pressure gradients - Turbulent boundary layer - Reynolds equation
Edition Identifiers:
- The Open Library ID: OL19379518M
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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22Heat transfer and pressure drop performance of a finned-tube heat exchanger proposed for use in the NASA Lewis altitude wind tunnel
By G. James VanFossen
“Heat transfer and pressure drop performance of a finned-tube heat exchanger proposed for use in the NASA Lewis altitude wind tunnel” Metadata:
- Title: ➤ Heat transfer and pressure drop performance of a finned-tube heat exchanger proposed for use in the NASA Lewis altitude wind tunnel
- Author: G. James VanFossen
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1985
- Publish Location: [Cleveland, Ohio
“Heat transfer and pressure drop performance of a finned-tube heat exchanger proposed for use in the NASA Lewis altitude wind tunnel” Subjects and Themes:
- Subjects: ➤ Cloud glaciation - Cooling fins - Heat exchangers - Heat transfer - High altitude - Ice formation - Lewis Research Center - Pressure gradients - Sprayers - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL16151468M
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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Find Heat transfer and pressure drop performance of a finned-tube heat exchanger proposed for use in the NASA Lewis altitude wind tunnel at online marketplaces:
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23Control of separated flow past a cylinder using tangential wall jet blowing
By Sejong Oh
“Control of separated flow past a cylinder using tangential wall jet blowing” Metadata:
- Title: ➤ Control of separated flow past a cylinder using tangential wall jet blowing
- Author: Sejong Oh
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1989
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Control of separated flow past a cylinder using tangential wall jet blowing” Subjects and Themes:
- Subjects: ➤ Circular cylinders - Fluid dynamics - Separated flow - Airfoils - Pressure gradients - Wall jets - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15409350M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
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24Experimental feasibility of investigating acoustic waves in Couette flow with entropy and pressure gradients
By Tony L. Parrott
“Experimental feasibility of investigating acoustic waves in Couette flow with entropy and pressure gradients” Metadata:
- Title: ➤ Experimental feasibility of investigating acoustic waves in Couette flow with entropy and pressure gradients
- Author: Tony L. Parrott
- Language: English
- Number of Pages: Median: 50
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“Experimental feasibility of investigating acoustic waves in Couette flow with entropy and pressure gradients” Subjects and Themes:
- Subjects: ➤ Sound waves - Resonant frequencies - Pressure gradients - Couette flow - Temperature gradients - Entropy - Waves - Vibration mode
Edition Identifiers:
- The Open Library ID: OL16132178M
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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25Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers
By Meelan Choudhari
“Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers” Metadata:
- Title: ➤ Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers
- Author: Meelan Choudhari
- 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
“Acoustic receptivity due to weak surface inhomogeneities in adverse pressure gradient boundary layers” Subjects and Themes:
- Subjects: ➤ Laminar boundary layer - Sound waves - Reynolds number - Pressure gradients - Falkner-Skan equation - Transition flow - Boundary-layer transition
Edition Identifiers:
- The Open Library ID: OL17114865M
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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26Effect of crossflow on Görtler instability in incompressible boundary layers
By Y. H. Zurigat
“Effect of crossflow on Görtler instability in incompressible boundary layers” Metadata:
- Title: ➤ Effect of crossflow on Görtler instability in incompressible boundary layers
- Author: Y. H. Zurigat
- Language: English
- Publisher: ➤ Institute for Computer Applications in Science and Engineering, NASA Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: [Springfield, Va - Hampton, VA
“Effect of crossflow on Görtler instability in incompressible boundary layers” Subjects and Themes:
- Subjects: ➤ Sweep angle - Incompressible boundary layer - Boundary layer stability - Cross flow - Boundary layer flow - Goertler instability - Pressure gradients - Reynolds number - Three dimensional boundary layer - Critical velocity
Edition Identifiers:
- The Open Library ID: OL15409991M
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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27Trailing edge flow conditions as a factor in airfoil design
By A. I. Ormsbee
“Trailing edge flow conditions as a factor in airfoil design” Metadata:
- Title: ➤ Trailing edge flow conditions as a factor in airfoil design
- Author: A. I. Ormsbee
- Language: English
- Publisher: ➤ Aeronautical and Astronautical Engineering Dept., University of Illinois - National Aeronautics and Space Administration
- Publish Date: 1984
- Publish Location: [Washington, DC - Urbana, Ill
“Trailing edge flow conditions as a factor in airfoil design” Subjects and Themes:
- Subjects: ➤ Pressure gradients - Trailing edges (Aerodynamics) - Design and construction - Trailing edges - Airfoils - Aircraft design - Potential flow - Aerofoils
Edition Identifiers:
- The Open Library ID: OL16153716M
Access and General Info:
- First Year Published: 1984
- 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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28Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation
By Klaus Rued
“Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation” Metadata:
- Title: ➤ Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation
- Author: Klaus Rued
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1987
- Publish Location: ➤ [Springfield, Va - Washington, D. C
“Transitional boundary layers under the influence of high free stream turbulence, intensive wall cooling and high pressure gradinets in hot gas circulation” Subjects and Themes:
- Subjects: ➤ Surface cooling - Turbulent boundary layer - Boundary layer transition - Pressure gradients - Gas flow - Free flow
Edition Identifiers:
- The Open Library ID: OL15417348M
Access and General Info:
- First Year Published: 1987
- 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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