Nozzles and thrust

The converging-diverging nozzle, expansion ratio, and altitude compensation.

Scope

• Isentropic flow and the thrust equation
• Expansion ratio and the optimum-expansion condition
• Overexpansion, underexpansion and flow separation
• Aerospikes and altitude-compensating designs

Notes

Nothing written here yet. Working notes go in Research and Learning Lab; anything that becomes durable is promoted onto this page.

References

To be added as the topic is worked through.