Pressure variations in rocket nozzles. Part 3: Direct calculation of the local Mach number

Keyphrases

• Mach number 100%
• Pressure Variation 100%
• Rocket Nozzle 100%
• Direct Calculation 100%
• Specific Heat Ratio 66%
• Speed of Sound 33%
• Order of Accuracy 33%
• Successive Approximation 33%
• Attendants 33%
• Area Ratio 33%
• Inversion Method 33%
• Classical Analysis 33%
• Local Velocity 33%
• Closed-form Representation 33%
• Numerical Root Finding 33%
• Supersonic Nozzle 33%
• Analytical Inversion 33%
• Subsonic Solutions 33%
• Number Expressions 33%
• Selective Extraction 33%
• Recursive Formulation 33%

Engineering

• Mach Number 100%
• Closed Form 33%
• Cross Section 33%
• Recursive 33%
• Successive Approximation 33%
• Area Ratio 33%
• Local Velocity 33%