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Crucigrama Sopa de Letras Hoja de Trabajo
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Advanced Prop

Solution
Horizontales
Inlet flow adjusts to demand.
Simple ducting
Opposite of Convergent
Aerodynamic forcing causes cycle stresses
For Compressor station 3-3R
How compressors work equation
Low airflow
Pressure difference between suction and pressure sides of the blades and stators
Difficult achieving efficient, stable supersonic diffusion over a wide mach range
Accounts for the boundary layer; uses nozzle geo. to predict losses instead of using pi_n
Accounts for thrust loss due to non-axial flow out of the nozzle.
Self-induced vibration that occurs if a flow-induced forcing function.
Verticales
Installation loss at inlet
To bring air required by the engine from free stream.
M_max = 1 at exit for nozzle
Momentum loss due tp wall friction in the nozzle.
What all the parts we learned make :)
Yourself
Coefficient of ratio of the 1-D area from cycle calculation for the nozzle throat
Work as much as the compressor needs
Between compressor stations 1-2R