Classical studies of the dynamics of compressible media incorporate the pos
sibility of exothermic actions in the field via the use of model combustion
waves treated as discontinuous, and hence quasi-steady, phenomena. The lat
ter are familiar under their broad titles of plane detonation waves; which
travel at supersonic speeds, and deflagrations, which travel subsonically.
Such deflagrations are not like conventional premixed flames insofar as lam
inar heat conduction and mass diffusion have no part to play in them. it is
convenient to categorize these combustion waves as diffusionless.
With the inclusion of adiabatic shock waves and contact discontinuities, a
whole range of formally unsteady phenomena can be analysed with the aid of
these discontinuous combustion-wave models. Such skeletal theoretical ideas
can be instructive; but they do suffer from a serious difficulty since the
y do not relate speeds of propagation of the combustion waves to the local
environments that they inhabit, and it is necessary to call on empirical ev
idence to close the theory.
The present paper shows that these difficulties can be overcome by adopting
an asymptotic parameter-perturbation approach to the construction of a sel
f-contained rational theory of diffusionless combustion. It is demonstrated
that asymptotic ideas are intrinsic to the classical studies of gas dynami
cs. Then logical pursuit of asymptotic thinking helps to consolidate the th
eory into a complete and consistent form, banishes the need for empiricism
and sheds light on the physics of compressible reacting flows. The latter i
s exemplified here with an examination of the ephemeral character of weak d
etonations and their role in the birth of strong detonation waves.