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Author: Arthur Leslie Jones
Publisher:
Published: 1949
Total Pages: 72
ISBN-13:
DOWNLOAD EBOOKThe variation of the yawing moment with sideslip and the variation of the stability derivative with aspect ratio and Mach number were investigated.
Author: Arthur L. Jones
Publisher:
Published: 1948
Total Pages: 644
ISBN-13:
DOWNLOAD EBOOKThe variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1951
Total Pages: 654
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1950
Total Pages: 440
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1949
Total Pages: 694
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1948
Total Pages: 446
ISBN-13:
DOWNLOAD EBOOKAuthor: Seymour Lampert
Publisher:
Published: 1951
Total Pages: 64
ISBN-13:
DOWNLOAD EBOOKA method is presented for determining the rolling and yawing moments of swept-back wings in steady sideslip at supersonic speeds. The case treated in particular is that of a swept tapered wing with all edges subsonic.
Author: W. E. Moeckel
Publisher:
Published: 1949
Total Pages: 674
ISBN-13:
DOWNLOAD EBOOKApplication of the method of characteristics to the linearized three-dimensional equation results in a relatively simple system of difference equations that can be used to compute the supersonic flow past boundaries for which no other linearized solutions are available.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1952
Total Pages: 498
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1949
Total Pages: 664
ISBN-13:
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