- 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.