Effects of Sweep Angle on the Boundary-layer Stability Characteristics of an Untapered Wing at Low Speeds

Effects of Sweep Angle on the Boundary-layer Stability Characteristics of an Untapered Wing at Low Speeds PDF Author: Frederick W. Boltz
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 86

Get Book

Book Description

Effects of Sweep Angle on the Boundary-layer Stability Characteristics of an Untapered Wing at Low Speeds

Effects of Sweep Angle on the Boundary-layer Stability Characteristics of an Untapered Wing at Low Speeds PDF Author: Frederick W. Boltz
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 86

Get Book

Book Description


Effects of Sweep Angle on the Boundary-layer Stability Characteristics of an Untapered Wing at Low Speeds

Effects of Sweep Angle on the Boundary-layer Stability Characteristics of an Untapered Wing at Low Speeds PDF Author: Frederick W. Boltz
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

Get Book

Book Description


NASA Reference Publication

NASA Reference Publication PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 984

Get Book

Book Description


Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate

Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate PDF Author: Don W. Jillie
Publisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36

Get Book

Book Description


Theoretical and Computational Aerodynamics

Theoretical and Computational Aerodynamics PDF Author: Tapan K. Sengupta
Publisher: John Wiley & Sons
ISBN: 1118787595
Category : Technology & Engineering
Languages : en
Pages : 544

Get Book

Book Description
Aerodynamics has seen many developments due to the growth of scientific computing, which has caused the design cycle time of aerospace vehicles to be heavily reduced. Today computational aerodynamics appears in the preliminary step of a new design, relegating costly, time-consuming wind tunnel testing to the final stages of design. Theoretical and Computational Aerodynamics is aimed to be a comprehensive textbook, covering classical aerodynamic theories and recent applications made possible by computational aerodynamics. It starts with a discussion on lift and drag from an overall dynamical approach, and after stating the governing Navier-Stokes equation, covers potential flows and panel method. Low aspect ratio and delta wings (including vortex breakdown) are also discussed in detail, and after introducing boundary layer theory, computational aerodynamics is covered for DNS and LES. Other topics covered are on flow transition to analyse NLF airfoils, bypass transition, streamwise and cross-flow instability over swept wings, viscous transonic flow over airfoils, low Reynolds number aerodynamics, high lift devices and flow control. Key features: Blends classical theories of incompressible aerodynamics to panel methods Covers lifting surface theories and low aspect ratio wing and wing-body aerodynamics Presents computational aerodynamics from first principles for incompressible and compressible flows Covers unsteady and low Reynolds number aerodynamics Includes an up-to-date account of DNS of airfoil aerodynamics including flow transition for NLF airfoils Contains chapter problems and illustrative examples Accompanied by a website hosting problems and a solution manual Theoretical and Computational Aerodynamics is an ideal textbook for undergraduate and graduate students, and is also aimed to be a useful resource book on aerodynamics for researchers and practitioners in the research labs and the industry.

NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 54

Get Book

Book Description


Viscous Drag Reduction in Boundary Layers

Viscous Drag Reduction in Boundary Layers PDF Author:
Publisher: AIAA
ISBN: 9781600863783
Category : Boundary layer
Languages : en
Pages : 542

Get Book

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 794

Get Book

Book Description


Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 1196

Get Book

Book Description


Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :

Get Book

Book Description