Real Gas Flow Tables for Nondissociated Air
Author : Louis G. Kaufman
Publisher :
Page : 272 pages
File Size : 33,24 MB
Release : 1959
Category : Air
ISBN :
Author : Louis G. Kaufman
Publisher :
Page : 272 pages
File Size : 33,24 MB
Release : 1959
Category : Air
ISBN :
Author : D. E. Randall
Publisher :
Page : 36 pages
File Size : 37,35 MB
Release : 1961
Category : Aerothermodynamics
ISBN :
This report presents a list of references which provide tabulated or graphical information regarding the atmosphere, gas flows, flow through shock waves, and information on the thermodynamic and transport properties of gases.
Author : Ali Bulent Cambel
Publisher :
Page : 184 pages
File Size : 30,55 MB
Release : 1963
Category : Science
ISBN :
Author :
Publisher :
Page : 216 pages
File Size : 46,34 MB
Release : 1962
Category : Science
ISBN :
Author :
Publisher :
Page : 36 pages
File Size : 40,36 MB
Release : 1961
Category : Nuclear energy
ISBN :
Author :
Publisher :
Page : 160 pages
File Size : 50,79 MB
Release : 1989
Category : Compressibility
ISBN :
Author :
Publisher :
Page : 906 pages
File Size : 15,88 MB
Release : 1969
Category : Engineering
ISBN :
Author : Society of Automotive Engineers
Publisher :
Page : 1024 pages
File Size : 43,54 MB
Release : 1962
Category : Airplanes
ISBN :
Author :
Publisher :
Page : 1722 pages
File Size : 28,55 MB
Release : 1962
Category : Research
ISBN :
Author : Victor L. Peterson
Publisher :
Page : 44 pages
File Size : 46,74 MB
Release : 1965
Category : Planets
ISBN :
Equations for aerodynamic quantities of interest in equilibrium isentropic one-dimensional flows and for properties across plane showck waves in arbitrary of planetary gases are derived under the assumption that the gases obey the perfect gas law. This assumption restricts the range of applicability of the equations to conditions for which the onset of chemical dissociation or ionization has not been reached although no requirement for the gases to be calorically perfect is imposed. Analytic functions used to specify the variation of specific heats with temperature are consistent with the assumption that molecular vibrations behave like harmonic oscillators and are independent of rotational degrees of freedom. Simplified equations giving approximate results over more limited ranges of the variables are also presented. Sample comparisons of the aerodynamic behavior of a number of pure gases are made. It is shown that while some of the flow quantities characterizing aerodynamic flows are very sensitive to gas composition, the stagnation pressure coefficients for a number of gases differ by only a few percent from one gas to another.