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Author: Harry A. Williams
Publisher:
Published: 1951
Total Pages: 70
ISBN-13:
DOWNLOAD EBOOKSImilar tests of an exploratory nature were made with angle cross section beams. A modification of Cozzone's method gave reasonable results for some positions of loading but not for others.
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Publisher:
Published: 1951
Total Pages: 38
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DOWNLOAD EBOOKAuthor:
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Published: 1973
Total Pages: 568
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DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1952
Total Pages: 498
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1949
Total Pages: 750
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1954
Total Pages: 162
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DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1951
Total Pages: 1078
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DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1951
Total Pages: 560
ISBN-13:
DOWNLOAD EBOOKAuthor: James C. Sivells
Publisher:
Published: 1951
Total Pages: 722
ISBN-13:
DOWNLOAD EBOOKA method is presented for calculating lift distributions for unswept wings with flaps or ailerons using nonlinear section lift data. This method is based upon lifting-line theory and is an extension to the method described by NACA Report 865. Simplified computing forms containing detailed examples are given for both symmetrical and asymmetrical lift distributions. A few comparisons of experimental and calculated characteristics are also presented.
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Publisher:
Published: 1951
Total Pages: 1376
ISBN-13:
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