- Author
- Smith, A. G.
- Title
- Theory of Resonant Burning of Solid Propellants Assuming a Constant Surface Temperature.
- Report
- A.R.C.21.018, May 12, 1959, 13 p.
- Keywords
- solid propellants | surface temperature | burning rate | pressure | combustion chambers | temperature distribution
- Abstract
- The fundamental idea of the present theory is that the solid propellant gasifies immediately it reaches a fixed temperature. The main deduction from the theory is that the only useful attack on resonant burning is by damping the modes in more or less well known ways.