Measurement of Particle Drag Coefficients in Flow Regimes Encountered by Particles in a Rocket Nozzle
Final technical rept. 1 Sep 1967-28 Feb 1969
UNITED TECHNOLOGY CENTER SUNNYVALE CA
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An experimental investigation was conducted to determine the drag coefficient of particles in flow regimes encountered in a rocket nozzle. The acquisition of these data leads to more reliable predictions of nozzle performance inefficiencies owing to gas-particle flow. The Mach number-Reynolds number regime traversed by a particle in a rocket nozzle is described.
- Fluid Mechanics
- Solid Propellant Rocket Engines