By Brian Randell
ALGOL 60 implementation: the interpretation and use of ALGOL 60 courses on a computer
Volume five of A.P.I.C. stories in facts processing
Issue five of ALGOL 60 Implementation, Brian Randell
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Extra info for ALGOL 60 Implementation: The Translation and Use of ALGOL 60 Programs on a Computer
TD = Π ¯ t − DF K0 Π t t Σ¯ d = Σ¯ − K0 I + F t · dF K0 σ¯ tD = σ¯ t − Kt I + f t · D f Kt π¯ td = π¯ t − d f Kt . 67) Correspondingly, the additive decomposition of the volume forces bτ and Bτ is likewise valid ¯ τ. 14) reveals the following identities. 47). 6 Balance of energy The balance of total energy as a representation of the first law of thermodynamics balances the rate of change of the volume specific total energy density Eτ = ρτ E as the sum of the kinetic and internal energy density Eτ = Kτ + Iτ with the external power.
In both cases, the apparent changes in mass result from confining attention to only a part of the overall matter present. Thus one might argue, that these problems can be overcome naturally by using the ’theory of mixtures’, as proposed by Truesdell & Toupin  §155 or Bowen . Therein, the loss or gain of mass of one constituent is compensated by the others while the mass of the overall mixture itself remains constant. e. the outside world. This approach typically falls within the category of ’thermodynamics of open systems’.
Open From the above equations, the reduced open system force term f¯ , which is responsible for the rocket thrust, can be identified as the force caused by the difference of the velocity of the ejection v¯ with respect to the rocket head velocity v. 6) 21 3 Balance equations Note that in the literature, the propulsive term [ v¯ − v ] R is sometimes also referred to as ’irreversible’ contribution while the extra force v R generated by the ejection leaving the system at the same velocity as the remaining rocket head is then denoted as ’reversible’ contribution.