Aeronautics & Astronautics - Fluid & Thermal Sciences > Rocket Propulsion: Page 1

No. 29150 Burn surface contours in cylindrical 2-dimensional grain with 2 slots No. 29162 Combustion flame structure of a double-base propellant No. 29163 Ignition pressure transient portion: motor chamber pressure-time trace No. 29164 Propellant ignitability curves No. 29165 Combustion instability of rocket motor: pressure-time history No. 29166 Period of combustion instability of rocket motor No. 29167 Period of combustion instability of rocket motor No. 28998 Liquid propellant rocket engine with gas pressure feed system No. 28999 Liquid propellant rocket engine with turbopump feed system No. 29000 Altitude performance of RS-27 rocket engine No. 29001 Energy balance of a chemical rocket No. 29002 Propulsive efficiency at different velocities No. 29003 Acceleration in multiples of earth gravity No. 29004 Total dynamic pressure for an incompressible fluid No. 29005 Plate moving in the direction of flow No. 29006 Area ratio to Mach Number Relation for isentropic flow No. 29007 Change of Ideal Cycle Efficiency with pressure ratio No. 29008 Specific exhaust velocity and impulse No. 29009 Typical variation of cross-section area in a rocket nozzle No. 29010 Variation of area & temperature with velocity in a rocket nozzle No. 29011 Typical variation of velocity with pressure in a rocket nozzle No. 29012 Typical variation of Mach number with pressure in a rocket nozzle No. 29013 Typical variation of specific volume with pressure in a rocket nozzle No. 29014 Typical variation of velocity with pressure in a rocket nozzle No. 29015 Nozzle shape for inducing subsonic flow No. 29016 Nozzle shape for inducing sonic flow No. 29017 Nozzle shape for inducing supersonic flow No. 29018 Area & velocity ratios vs pressure ratio: Supersonic nozzle No. 29019 Area & velocity ratios vs pressure ratio: Supersonic nozzle No. 29020 Thrust coefficient vs pressure, nozzle area and specific heat ratios No. 29021 Coefficient's thrust vs ratio's nozzle area No. 29022 Pressure distribution in a convergent-divergent nozzle No. 29023 Nozzles' thrust coefficients with different area ratios No. 29024 Nozzle behavior during flight (booster or first stage) No. 29025 Nozzle behavior during sealevel static tests (booster or first stage) No. 29026 Nozzle behavior during flight (second stage) No. 29027 Nozzle behavior during sealevel static tests (second stage) No. 29028 Nozzle behavior during flight (third stage) No. 29029 Nozzle behavior during sealevel static tests (third stage) No. 29030 Comparison of length for various types of nozzles No. 29031 Temperature variation in cooled rocket thrust chamber No. 29032 Typical temperature-time-location history No. 29033 Partially submerged nozzle design for a solid propellant motor No. 29034 External nozzle design for a solid propellant motor No. 29035 Method for forming a cool boundary layer in a rocket nozzle No. 29036 Method for forming a cool boundary layer in a rocket nozzle No. 29037 Method for forming a cool boundary layer in a rocket nozzle No. 29038 Regimes for heat transfer from a hot wall to a flowing liquid No. 29039 Maximum missile velocity vs specific impulse in zero gravity space
 

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