Experimental and Analytical Investigation of Flutter of a Nonuniform Sweptback Cantilever Wing with Two Concentrated Weights

Experimental and Analytical Investigation of Flutter of a Nonuniform Sweptback Cantilever Wing with Two Concentrated Weights PDF Author: John L. Sewall
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38

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Experimental and Analytical Investigation of Flutter of a Nonuniform Sweptback Cantilever Wing with Two Concentrated Weights

Experimental and Analytical Investigation of Flutter of a Nonuniform Sweptback Cantilever Wing with Two Concentrated Weights PDF Author: John L. Sewall
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 38

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 836

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Determination of Influence Coefficients

Determination of Influence Coefficients PDF Author: S. Levy
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ISBN:
Category : Airplanes
Languages : en
Pages : 642

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Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 516

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Report

Report PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 644

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Journal of the Royal Aeronautical Society

Journal of the Royal Aeronautical Society PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 992

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On Possible Similarity Solutions for Three-dimensional Incompressible Laminar Boundary Layers

On Possible Similarity Solutions for Three-dimensional Incompressible Laminar Boundary Layers PDF Author: Arthur G. Hansen
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ISBN:
Category : Air flow
Languages : en
Pages : 716

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Book Description
Solutions of mainstream flow patterns for all possible incompressible laminar-boundary-layer flows having classical similarity with respect to rectangular coordinate systems are derived. These solutions, which apply to a wide range of flows, are summarized in table form.

Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category :
Languages : en
Pages : 596

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Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4

Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4 PDF Author: C. H. Wilts
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ISBN:
Category : Aeronautics
Languages : en
Pages : 358

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Technical Memorandum - National Advisory Committee for Aeronautics

Technical Memorandum - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 632

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Book Description
Chiefly translations from foreign aeronautical journals.