Discover our new portal: your complete exam preparation, enhanced by AI

Login Start Now

Home > Exam Questions > ATPL - Airline Transport Pilot license > Principles of Flight > In case of supersonic flow retarded by a normal shock wave a high efficiency (low loss in total pressure) can be obtained if the Mach number in front of the shock is

325 - ATPL - In case of supersonic flow retarded by a normal shock wave a high efficiency (low loss in total pressure) can be obtained if the Mach number in front of the shock is

Question 325 - Principles of Flight - ATPL - Airline Transport Pilot license

Lower than 1.

High (supersonic).

Exactly 1.

Small but still supersonic.

This is 1 of over 400 exam questions on Principles of Flight

Take a test with 10 questions

Training tests and timed exam simulations ATPL - Airline Transport Pilot license

Principles of Flight Training! PRO Question explanation