A Three-Dimensional, Compressible, Laminar Boundary-Layer Method for General Fuselages. Volume 1: Numerical Method

A Three-Dimensional, Compressible, Laminar Boundary-Layer Method for General Fuselages. Volume 1: Numerical Method PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781731094674
Category : Science
Languages : en
Pages : 122

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Book Description
A procedure for calculating 3-D, compressible laminar boundary layer flow on general fuselage shapes is described. The boundary layer solutions can be obtained in either nonorthogonal 'body oriented' coordinates or orthogonal streamline coordinates. The numerical procedure is 'second order' accurate, efficient and independent of the cross flow velocity direction. Numerical results are presented for several test cases, including a sharp cone, an ellipsoid of revolution, and a general aircraft fuselage at angle of attack. Comparisons are made between numerical results obtained using nonorthogonal curvilinear 'body oriented' coordinates and streamline coordinates. Wie, Yong-Sun Unspecified Center BOUNDARY LAYER FLOW; COMPRESSIBLE BOUNDARY LAYER; COMPUTATIONAL FLUID DYNAMICS; FUSELAGES; LAMINAR BOUNDARY LAYER; THREE DIMENSIONAL BOUNDARY LAYER; ANGLE OF ATTACK; COMPUTER PROGRAMS; CONES; COORDINATES; CROSS FLOW; ELLIPSOIDS...

A Three-Dimensional, Compressible, Laminar Boundary-Layer Method for General Fuselages. Volume 1: Numerical Method

A Three-Dimensional, Compressible, Laminar Boundary-Layer Method for General Fuselages. Volume 1: Numerical Method PDF Author: National Aeronautics and Space Adm Nasa
Publisher: Independently Published
ISBN: 9781731094674
Category : Science
Languages : en
Pages : 122

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Book Description
A procedure for calculating 3-D, compressible laminar boundary layer flow on general fuselage shapes is described. The boundary layer solutions can be obtained in either nonorthogonal 'body oriented' coordinates or orthogonal streamline coordinates. The numerical procedure is 'second order' accurate, efficient and independent of the cross flow velocity direction. Numerical results are presented for several test cases, including a sharp cone, an ellipsoid of revolution, and a general aircraft fuselage at angle of attack. Comparisons are made between numerical results obtained using nonorthogonal curvilinear 'body oriented' coordinates and streamline coordinates. Wie, Yong-Sun Unspecified Center BOUNDARY LAYER FLOW; COMPRESSIBLE BOUNDARY LAYER; COMPUTATIONAL FLUID DYNAMICS; FUSELAGES; LAMINAR BOUNDARY LAYER; THREE DIMENSIONAL BOUNDARY LAYER; ANGLE OF ATTACK; COMPUTER PROGRAMS; CONES; COORDINATES; CROSS FLOW; ELLIPSOIDS...

A Three-Dimensional, Compressible, Laminar Boundary-Layer Method for General Fuselages. Volume 1

A Three-Dimensional, Compressible, Laminar Boundary-Layer Method for General Fuselages. Volume 1 PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722913458
Category :
Languages : en
Pages : 120

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Book Description
A procedure for calculating 3-D, compressible laminar boundary layer flow on general fuselage shapes is described. The boundary layer solutions can be obtained in either nonorthogonal 'body oriented' coordinates or orthogonal streamline coordinates. The numerical procedure is 'second order' accurate, efficient and independent of the cross flow velocity direction. Numerical results are presented for several test cases, including a sharp cone, an ellipsoid of revolution, and a general aircraft fuselage at angle of attack. Comparisons are made between numerical results obtained using nonorthogonal curvilinear 'body oriented' coordinates and streamline coordinates. Wie, Yong-Sun Unspecified Center BOUNDARY LAYER FLOW; COMPRESSIBLE BOUNDARY LAYER; COMPUTATIONAL FLUID DYNAMICS; FUSELAGES; LAMINAR BOUNDARY LAYER; THREE DIMENSIONAL BOUNDARY LAYER; ANGLE OF ATTACK; COMPUTER PROGRAMS; CONES; COORDINATES; CROSS FLOW; ELLIPSOIDS...

A Three-dimensional, Compressible, Laminar Boundary-layer Method for General Fuselages. Volume 2: User's Manual

A Three-dimensional, Compressible, Laminar Boundary-layer Method for General Fuselages. Volume 2: User's Manual PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 172

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Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 652

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Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
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ISBN:
Category : Government publications
Languages : en
Pages : 1830

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
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Category : Government publications
Languages : en
Pages : 1118

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BLSTA - a Boundary Layer Code for Stability Analysis

BLSTA - a Boundary Layer Code for Stability Analysis PDF Author: Yong-Sun Wie
Publisher:
ISBN:
Category : Laminar boundary layer
Languages : en
Pages : 120

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Cities and Their Vital Systems

Cities and Their Vital Systems PDF Author: Advisory Committee on Technology and Society
Publisher: National Academies Press
ISBN: 9780309037860
Category : Social Science
Languages : en
Pages : 1298

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Book Description
Cities and Their Vital Systems asks basic questions about the longevity, utility, and nature of urban infrastructures; analyzes how they grow, interact, and change; and asks how, when, and at what cost they should be replaced. Among the topics discussed are problems arising from increasing air travel and airport congestion; the adequacy of water supplies and waste treatment; the impact of new technologies on construction; urban real estate values; and the field of "telematics," the combination of computers and telecommunications that makes money machines and national newspapers possible.

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Government Reports Announcements & Index PDF Author:
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Category : Science
Languages : en
Pages : 650

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NASA SP.

NASA SP. PDF Author:
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Category : Aeronautics
Languages : en
Pages : 548

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