Author: Colin Phillip Coleman
Publisher:
ISBN:
Category :
Languages : en
Pages : 212
Book Description
Boundary Layer Transition in the Leading Edge Region of a Swept Cylinder in High Speed Flow
Author: Colin Phillip Coleman
Publisher:
ISBN:
Category :
Languages : en
Pages : 212
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 212
Book Description
Blsta
Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722959685
Category :
Languages : en
Pages : 118
Book Description
A computer program is developed to solve the compressible, laminar boundary-layer equations for two-dimensional flow, axisymmetric flow, and quasi-three-dimensional flows including the flow along the plane of symmetry, flow along the leading-edge attachment line, and swept-wing flows with a conical flow approximation. The finite-difference numerical procedure used to solve the governing equations is second-order accurate. The flow over a wide range of speed, from subsonic to hypersonic speed with perfect gas assumption, can be calculated. Various wall boundary conditions, such as wall suction or blowing and hot or cold walls, can be applied. The results indicate that this boundary-layer code gives velocity and temperature profiles which are accurate, smooth, and continuous through the first and second normal derivatives. The code presented herein can be coupled with a stability analysis code and used to predict the onset of the boundary-layer transition which enables the assessment of the laminar flow control techniques. A user's manual is also included. Wie, Yong-Sun Unspecified Center APPLICATIONS PROGRAMS (COMPUTERS); AXISYMMETRIC FLOW; BOUNDARY LAYER FLOW; BOUNDARY LAYER STABILITY; CONICAL FLOW; FINITE DIFFERENCE THEORY; LAMINAR BOUNDARY LAYER; LEADING EDGES; STABILITY TESTS; SWEPT WINGS; TWO DIMENSIONAL FLOW; USER MANUALS (COMPUTER PROGRAMS); BOUNDARY CONDITIONS; BOUNDARY LAYER CONTROL; BOUNDARY LAYER TRANSITION; COMPUTATIONAL FLUID DYNAMICS; HYPERSONIC SPEED; IDEAL GAS; SUBSONIC SPEED...
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722959685
Category :
Languages : en
Pages : 118
Book Description
A computer program is developed to solve the compressible, laminar boundary-layer equations for two-dimensional flow, axisymmetric flow, and quasi-three-dimensional flows including the flow along the plane of symmetry, flow along the leading-edge attachment line, and swept-wing flows with a conical flow approximation. The finite-difference numerical procedure used to solve the governing equations is second-order accurate. The flow over a wide range of speed, from subsonic to hypersonic speed with perfect gas assumption, can be calculated. Various wall boundary conditions, such as wall suction or blowing and hot or cold walls, can be applied. The results indicate that this boundary-layer code gives velocity and temperature profiles which are accurate, smooth, and continuous through the first and second normal derivatives. The code presented herein can be coupled with a stability analysis code and used to predict the onset of the boundary-layer transition which enables the assessment of the laminar flow control techniques. A user's manual is also included. Wie, Yong-Sun Unspecified Center APPLICATIONS PROGRAMS (COMPUTERS); AXISYMMETRIC FLOW; BOUNDARY LAYER FLOW; BOUNDARY LAYER STABILITY; CONICAL FLOW; FINITE DIFFERENCE THEORY; LAMINAR BOUNDARY LAYER; LEADING EDGES; STABILITY TESTS; SWEPT WINGS; TWO DIMENSIONAL FLOW; USER MANUALS (COMPUTER PROGRAMS); BOUNDARY CONDITIONS; BOUNDARY LAYER CONTROL; BOUNDARY LAYER TRANSITION; COMPUTATIONAL FLUID DYNAMICS; HYPERSONIC SPEED; IDEAL GAS; SUBSONIC SPEED...
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
04-2527 - 04-2554
Author:
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 442
Book Description
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 442
Book Description
CFD-based Aircraft Drag Prediction and Reduction
Author: H. Deconinck
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 742
Book Description
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 742
Book Description
Lecture series
Author:
Publisher:
ISBN:
Category : Fluid dynamic measurements
Languages : en
Pages : 744
Book Description
Publisher:
ISBN:
Category : Fluid dynamic measurements
Languages : en
Pages : 744
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1060
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1060
Book Description
Monthly Catalogue, United States Public Documents
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1060
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1060
Book Description
Transitional and Turbulent Compressible Flows
Author:
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 278
Book Description
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 278
Book Description
12th AIAA Applied Aerodynamics Conference
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 548
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 548
Book Description