Liquid Rocket Thrust Chambers
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23

(FIVE YEARS 0)

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2

(FIVE YEARS 0)

Published By American Institute Of Aeronautics And Astronautics

9781563472237, 9781600866760

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Subcritical/Supercritical Droplet Cluster Behavior in Dense and Dilute Regions of Sprays

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0323.0338 ◽

2004 ◽

pp. 323-338

Keyword(s):

Droplet Cluster ◽

Cluster Behavior

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Simulation and Analysis of Thrust Chamber Flowfields: Cryogenic Propellant Rockets

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0527.0551 ◽

2004 ◽

pp. 527-551

Keyword(s):

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Assessment of Thrust Chamber Performance

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0601.0620 ◽

2004 ◽

pp. 601-620 ◽

Keyword(s):

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Design and Dynamics of Jet and Swirl Injectors

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0019.0103 ◽

2004 ◽

pp. 19-103 ◽

Keyword(s):

Swirl Injectors

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Propellant Ignition and Flame Propagation

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0405.0435 ◽

2004 ◽

pp. 405-435 ◽

Keyword(s):

Flame Propagation

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Fundamentals of Supercritical Mixing and Combustion of Cryogenic Propellants

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0339.0367 ◽

2004 ◽

pp. 339-367 ◽

Keyword(s):

Cryogenic Propellants

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Simulation and Analysis of Thrust Chamber Flowfields: Storable Propellant Rockets

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0493.0525 ◽

2004 ◽

pp. 493-525

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Nozzle Design and Optimization

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0469.0492 ◽

2004 ◽

pp. 469-492 ◽

Keyword(s):

Nozzle Design ◽

Design And Optimization

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Thermodynamic Power Cycles for Pump-Fed Liquid Rocket Engines

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0621.0648 ◽

2004 ◽

pp. 621-648

Keyword(s):

Rocket Engines ◽

Power Cycles ◽

Liquid Rocket Engines ◽

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Table of Contents

Liquid Rocket Thrust Chambers ◽

10.2514/5.9781600866760.0000.0000 ◽

2004 ◽

pp. i-xx

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