Browsing Nr. 4 by Subject "aerospace propellants"

Sort by: Order: Results:

  • RUGESCU, R. D. (Editura U.T.M., 2005)
    The thermal freezing phenomenon was occasionally identified during an early experimental verification of shifting equilibrium rocket flow computations. The manner by which the value of 1671÷36ºK for this temperature was ...

Search DSpace


Browse

My Account