BOOK REVIEWS - Review of Turbulence -- An Introduction for Scientists and Engineers (Englisch)
- Neue Suche nach: Bradshaw, R.
- Neue Suche nach: Bradshaw, R.
In:
AIAA journal
;
43
, 2
; 446
;
2005
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ISSN:
- Aufsatz (Zeitschrift) / Print
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Titel:BOOK REVIEWS - Review of Turbulence -- An Introduction for Scientists and Engineers
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Beteiligte:Bradshaw, R. ( Autor:in )
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Erschienen in:AIAA journal ; 43, 2 ; 446
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Verlag:
- Neue Suche nach: AIAA
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Erscheinungsort:Reston, Va. [u.a.]
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Erscheinungsdatum:2005
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ISSN:
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ZDBID:
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Medientyp:Aufsatz (Zeitschrift)
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Format:Print
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Sprache:Englisch
- Neue Suche nach: 770/7040
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Schlagwörter:
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Klassifikation:
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Datenquelle:
Inhaltsverzeichnis – Band 43, Ausgabe 2
Zeige alle Jahrgänge und Ausgaben
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
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Euler Solution Using Cartesian Grid with a Gridless Least-Squares Boundary TreatmentE.P.C. Koh / Her-Mann Tsai / Feng Liu et al. | 2005
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Euler Solution Using Cartesian Grid with a Gridless Least-Squares Boundary TreatmentKoh, E.P.C. et al. | 2005
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Control of Edney IV Interaction by Pulsed Laser Energy DepositionRussell Adelgren / Hong Yan / Gregory Elliott / Doyle Knight / Thomas Beutner / Alexander Zheltovodov et al. | 2005
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Control of Edney IV Interaction by Pulsed Laser Energy DepositionAdelgren, R.G. et al. | 2005
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Reduced-Order Modeling of a Heaving AirfoilG. Lewin / H. Haj-Hariri et al. | 2005
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Reduced-Order Modeling of a Heaving AirfoilLewin, G.C. et al. | 2005
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Application of Simultaneous Perturbation Stochastic Approximation Method for Aerodynamic Shape Design OptimizationXiu Qing Xing / Murali Damodaran et al. | 2005
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Application of Simultaneous Perturbation Stochastic Approximation Method for Aerodynamic Shape Design OptimizationXing, X.Q. et al. | 2005
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AIRCRAFT TECHNOLOGY, CONVENTIONAL, STOL-VTOL - Calculation of Airfoil Flutter by an Euler Method with Approximate Boundary ConditionsGao, C. et al. | 2005
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Calculation of Airfoil Flutter by an Euler Method with Approximate Boundary ConditionsChao Gao / Shijun Luo / Feng Liu / David Schuster et al. | 2005
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ENERGY - Modeling Pulsed-Blowing Systems for Flow ControlKim, B.-H. et al. | 2005
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Modeling Pulsed-Blowing Systems for Flow ControlByung-Hun Kim / David Williams / Steve Emo / Mukund Acharya et al. | 2005
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FLUID DYNAMICS - Sound Generated by a Pair of Axisymmetric Coaxial Vortex RingsLiow, Y.S.K. et al. | 2005
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Sound Generated by a Pair of Axisymmetric viscous Coaxial Vortex Rings.Keith Liow / Mark Thompson / Kerry Hourigan et al. | 2005
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Sound Generated by a Pair of Axisymmetric Coaxial Vortex RingsLiow, Y. S. K. / Thompson, M. C. / Hourigan, K. et al. | 2005
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FLUID DYNAMICS - Evaluation of High-Order Spectral Volume Method for Benchmark Computational Aeroacoustic ProblemsWang, Z.J. et al. | 2005
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Numerical Investigation of Reflected Shock/Vortex Interaction near an Open-Ended DuctShen-Min Liang / Wen-Tai Chung / Hua Chen / Shiuh-Hwa Shyu et al. | 2005
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FLUID DYNAMICS - Numerical Investigation of Reflected Shock-Vortex Interaction near an Open-Ended DuctLiang, S.-M. et al. | 2005
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Reduced-Order Model for Efficient Simulation of Synthetic Jet ActuatorsNail Yamaleev / Mark Carpenter / Frederick Ferguson et al. | 2005
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FLUID DYNAMICS - Reduced-Order Model for Efficient Simulation of Synthetic Jet ActuatorsYamaleev, N.K. et al. | 2005
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Aerodynamic Performance of Transonic Bethe-Zel'dovich-Thompson Flows past an AirfoilCinnella, P. / Congedo, P. M. et al. | 2005
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FLUID DYNAMICS - Aerodynamic Performance of Transonic Bethe-Zel'dovich-Thompson Flows past an AirfoilCinnella, P. et al. | 2005
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Aerodynamic Performance of Transonic BetheZal'dovichThompson Flows past an AirfoilPaola Cinnella / Pietro Congedo et al. | 2005
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FLUID DYNAMICS - Penetration of a Transverse Supersonic Jet into a Subsonic Compressible CrossflowBeresh, S.J. et al. | 2005
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Penetration of a Transverse Supersonic Jet into a Subsonic Compressible CrossflowSteven Beresh / John Henfling / Rocky Erven / Russell Spillers et al. | 2005
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Experimental Investigation of a Pulse Detonation Engine with a Two-Dimensional EjectorDaniel Allgood / Ephraim Gutmark / Adam Rasheed / Anthony Dean et al. | 2005
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FLUID DYNAMICS - Experimental Investigation of a Pulse Detonation Engine with a Two-Dimensional EjectorAllgood, D. et al. | 2005
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Efficient Finite Difference Design SensitivitiesUri Kirsch / Michael Bogomolni / Fred van Keulen et al. | 2005
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Minimizing Blade Dynamic Response in a Bladed Disk Through Design OptimizationJianfu Hou / Charles Cross et al. | 2005
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PROPULSION AND POWER - Minimizing Blade Dynamic Response in a Bladed Disk Through Design OptimizationHou, J. et al. | 2005
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Direct Least-Squares Formulation of a Stiffness Adjustment MethodBrian Sako / Alvar Kabe et al. | 2005
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Effect of Pressure Distribution on Energy Dissipation in a Mechanical Lap JointYaxin Song / D. Michael McFarland / Lawrence Bergman / Alexander Vakakis et al. | 2005
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STRUCTURAL MECHANICS AND MATERIALS - Effect of Pressure Distribution on Energy Dissipation in a Mechanical Lap JointSong, Y. et al. | 2005
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Ballistic Perforation of Conically Cylindrical Steel Projectile into Three-Dimensional Braided CompositesBohong Gu / Yuling Li et al. | 2005
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STRUCTURAL MECHANICS AND MATERIALS - Ballistic Perforation of Conically Cylindrical Steel Projectile into Three-Dimensional Braided CompositesGu, B. et al. | 2005
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Aeroacoustic CarouselM C M Wright et al. | 2005
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Aeroacoustic Carousel (TN)Wright, M. C. M. et al. | 2005
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FLUID DYNAMICS - Decrease of the Effective Reynolds Number with Eddy-Viscosity Subgrid-Scale Modeling (TN)Bogey, C. et al. | 2005
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Decrease of the Effective Reynolds Number with Eddy-Viscosity Subgrid-Scale Modeling (TN)Bogey, C. / Bailly, C. et al. | 2005
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Decrease of the Effective Reynolds Number with Eddy-Viscosity Subgrid ModelingChristophe Bogey / Christophe Bailly et al. | 2005
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Damage Identification of Plate Structures Using a Hybrid Genetic-Sensitivity Approach (TN)Bland, S. M. / Kapania, R. K. et al. | 2005
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Damage Identification of Plate Structures Using a Hybrid Genetic-Sensitivity ApproachScott Bland / Rakesh Kapania et al. | 2005
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STRUCTURAL MECHANICS AND MATERIALS - Damage Identification of Plate Structures Using a Hybrid Genetic-Sensitivity Approach (TN)Bland, S.M. et al. | 2005
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STRUCTURAL MECHANICS AND MATERIALS - Buckling of a Circular Plate Weakened by Concentric Hinge or Partial Crack (TN)Wang, C.Y. et al. | 2005
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Buckling of a Circular Plate Weakened by Concentric Hinge or Partial Crack (TN)Wang, C. Y. et al. | 2005
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Buckling of a Circular Plate Weakened by Concentric Hinge or Partial CrackC.Y. Wang et al. | 2005
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