Abstract
The method developed by the author is adapted to the case of spherically symmetric gas motions. The pressure, density and velocity of the gas are shown to involve one arbitrary function Ф; if Ф =
f
(
t
)
w
(
rt
-α
), where
f
and
w
are arbitrary functions, explicit formulae for the pressure, density and velocity are worked out. Amongst motions of this kind, those in which the velocity is proportional to
r
, are selected for detailed investigation. Cases in which the gas motion is adiabatic are determined; in one type
w
is a known function of
rt
-α
, while
f
is the solution of a certain differential equation; in a second type,
f
is known but
w
remains arbitrary. Boundary conditions are then applied, first, on the assumption that the boundary is approximately a contact surface and that the motion is of the first type; secondly, when the boundary is a true shock surface and the motion has a special character and is common to both types. Primakoff's solution is obtained in the second case. The author’s method is contrasted with the conventional ones.
Reference5 articles.
1. Bondi H . 1952 Cosmology chap. IX . Cam bridge U niversity Press.
2. C ourant R . & Friedrichs K . O. 1948 Supersonic flow and shock waves. New Y ork: In te rscience Publishers.
3. K am ke E . 1943 Differentialglc ichungen: Losungsmethoden und Losungen 2nd ed. 1 24-26. Leipzig: B ecker u n d E rler Kom.-Ges.
4. McVittie G. C. 1953 Quart. A p p l. M ath. 11 327.
Cited by
29 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献