Boundary Layer Transition in the Leading Edge Region of a Swept Cylinder in High Speed Flow

Boundary Layer Transition in the Leading Edge Region of a Swept Cylinder in High Speed Flow PDF Author: Colin Phillip Coleman
Publisher:
ISBN:
Category :
Languages : en
Pages : 212

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Boundary Layer Transition in the Leading Edge Region of a Swept Cylinder in High Speed Flow

Boundary Layer Transition in the Leading Edge Region of a Swept Cylinder in High Speed Flow PDF Author: Colin Phillip Coleman
Publisher:
ISBN:
Category :
Languages : en
Pages : 212

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Blsta

Blsta PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722959685
Category :
Languages : en
Pages : 118

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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

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456

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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

04-2527 - 04-2554 PDF Author:
Publisher:
ISBN:
Category : Fluid dynamics
Languages : en
Pages : 442

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CFD-based Aircraft Drag Prediction and Reduction

CFD-based Aircraft Drag Prediction and Reduction PDF Author: H. Deconinck
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 742

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Lecture series

Lecture series PDF Author:
Publisher:
ISBN:
Category : Fluid dynamic measurements
Languages : en
Pages : 744

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1060

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1060

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Transitional and Turbulent Compressible Flows

Transitional and Turbulent Compressible Flows PDF Author:
Publisher:
ISBN:
Category : Compressibility
Languages : en
Pages : 278

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12th AIAA Applied Aerodynamics Conference

12th AIAA Applied Aerodynamics Conference PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 548

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