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Which of the following has begun flight testing electric vertical takeoff and landing (eVTOL) aircraft with Joby Aviation for air taxi services under its Advanced Air Mobility (AAM) National Campaign?
Fiat Chrysler has announced a partnership with which of the following to help lower costs and accelerate the launch of an electric “flying car,” more formally known as a vertical takeoff and landing (eVTOL) aircraft?
At which diameter we should design a supersonic after burning engine for a fighter which will have thrust at takeoff 150000 Unit and bypass ratio of 0.7.
In which state was India's first No-Permission No-Takeoff (NPNT) compliant drone flight on the A200 Remotely Piloted Aircraft System (RPAS) has been successfully completed?
What is the speed at which the takeoff is aborted when there is an engine failure?
Based on first order statistical jet engine model, we have been given a task to design a subsonic non afterburning engine which is operating at maximum Mach number of 0.7. Evaluate the approximate length required to build this engine. Given thrust at takeoff is 9600 unit.
Engine which can be estimated through statistical jet engine model has bypass ratio of 1.2 and maximum thrust at takeoff is 8000 Newton then what should be the design diameter for this engine. Consider a subsonic non after burning engine.
We need to design a supersonic fighter with afterburner which has maximum Mach number of 1.8. If thrust at takeoff is 10000 unit and bypass ratio is 0.71 then, find ratio of length to the diameter for this engine.
Calculate the approximate value of length at which supersonic after burning engine could be design in such a way that thrust at takeoff will be 29800 unit and maximum Mach number will be 2.12.
If our design has takeoff velocity of 120 knots then, at which value of stall speed we should design our aircraft?