The Linear Dynamics of a Turbojet Engine as Developed from the Linearized Component Equations
Author: Ross Dean Schmidt
Publisher:
Published: 1955
Total Pages: 242
ISBN-13:
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Author: Ross Dean Schmidt
Publisher:
Published: 1955
Total Pages: 242
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. National Advisory Committee for Aeronautics
Publisher:
Published: 1952
Total Pages: 408
ISBN-13:
DOWNLOAD EBOOKAuthor: Harold William Woolley
Publisher:
Published: 1956
Total Pages: 670
ISBN-13:
DOWNLOAD EBOOKTables are presented based on the Lennard-Jones 6-12 potential for nonpolar molecules to be used in the representation of second and third virial coefficients and equation-of-state corrections for enthalpy, entropy, specific heats at constant volume and at constant pressure, the ratio of specific heats, the isentropic expansion coefficient, and the velocity of sound. The treatment for effects involving three molecules jointly uses an empirical adjustment of the Lennard-Jones force parameters within a cluster of three independently of the value for an isolated pair. A graphical correlation of ratios of these parameters with the critical constants is also shown which permits better estimates for compact nonpolar molecules with known critical constants but with limited data of state.
Author:
Publisher:
Published: 1955
Total Pages: 236
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1957
Total Pages: 342
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1957
Total Pages: 488
ISBN-13:
DOWNLOAD EBOOKAuthor: University of Minnesota
Publisher:
Published: 1954
Total Pages: 354
ISBN-13:
DOWNLOAD EBOOKAuthor: Thomas R. Yechout
Publisher: AIAA
Published: 2003
Total Pages: 666
ISBN-13: 9781600860782
DOWNLOAD EBOOKBased on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.