• Question Tag: Supersonic flow
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• PollSupersonic flow has a Mach number

Supersonic flow has a Mach number

Asked on 29th June 2020 in
• 327 views
• How to mitigate the effect of  decrease in maximum  lift to drag ratio when there is increase in mach number.

How to mitigate the effect of  decrease in maximum  lift to drag ratio when there is increase in mach number.

Asked on 3rd July 2019 in
• 853 views
• What is swept wing ? How does wing sweep affects aircraft performance ?

What is swept wing ? How does wing sweep affects aircraft performance ?

Asked on 14th July 2020 in
• 626 views
• What angle does the Mach wave makes with the flow direction ?

An airplane flying at a Mach number of 2.2 makes a Mach wave at the nose. What angle does it …

Asked on 18th January 2021 in
• 613 views
• What is a Mach wave ?

What is a Mach wave ? How does it forms ?

Asked on 18th January 2021 in
• 669 views
• Calculate the wave drag on the wings of an airplane.

Calculate the wave drag on the wings of an airplane which is flying at a Mach number of $$2.1$$ at …

Asked on 18th January 2021 in
• 786 views
• What are shock waves ?

What are shock waves ? How does it originates ?

Asked on 18th January 2021 in
• 675 views
• What are expansion waves ?

What are expansion waves ? How does it originates ?

Asked on 18th January 2021 in
• 831 views
• Find $${P_2},{T_2},\,{\rho _2},\,{M_2},{P_{02}}$$ and $${T_{02}}$$ downstream of the shock wave.

A flow passes through a normal shock wave has a pressure, temperature and Mach number of  $$1\,atm,\,295\,K$$ and $$2.8$$ upstream …

Asked on 11th March 2021 in
• 359 views
An oblique shock wave is generated with a wave angle of $${30^ \circ }$$ in a Mach $$4$$ flow, at …