Bernoulli’s equation can be applied to compressible flow at which of the following matches the number?(a) mach number less than 1(b) mach number equal to 1(c) higher mach numbers(d) does not depends on mach numberThe question was asked by my school principal while I was bunking the class.This is a very interesting question from Bernoulli’s Equation in division Inviscid & Incompressible Flow of Aerodynamics

Bernoulli’s equation can be applied to compressible flow at which of

1.	Bernoulli’s equation can be applied to compressible flow at which of the following matches the number?(a) mach number less than 1(b) mach number equal to 1(c) higher mach numbers(d) does not depends on mach numberThe question was asked by my school principal while I was bunking the class.This is a very interesting question from Bernoulli’s Equation in division Inviscid & Incompressible Flow of Aerodynamics
Answer» Right option is (c) HIGHER mach numbers For EXPLANATION: Bernoulli’s principle states that increasing the velocity DECREASES the PRESSURE which gives us a higher lift. If the matches the number increases, gradually the pressure decreases which leads to an increase in lift.

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