• Question Cagtegory: Design
Filter by
Filter by
Questions Per Page:
• ## Find the reservoir pressure for a nozzle of a supersonic wind tunnel.

Find the reservoir pressure for a nozzle of a supersonic wind tunnel which has an exit-to-throat area ratio of $$4.441$$. …

Asked on 26th March 2021 in
• 133 views
• ## Symmetrical and cambered airfoil

What is the difference between symmetrical and asymmetrical /cambered airfoil ?

Asked on 17th December 2020 in
• 2K views
• ## PollWhen is the critical Mach number of an airfoil attained ?

The critical Mach number of an airfoil is attained when

Asked on 1st October 2019 in
• 279 views