Question: An aircraft is flying with wing loading of 50 and maximum CL as 2.4. If density is 1.225 then, find the stall speed of the aircraft.

Options

A : 5.832m/s

B : 5.823

C : 5.632m/s

D : 5.632

Click to view Correct Answer

Previous || Next

Wing Loading more questions

Which of the following is correct in accordance to diagram?^

Wing sweep is used to __

A civil A/C has maximum lift coefficient of 3. If....

A prop driven A/C has BHP/W as 0.08. If density....

An aircraft has catapult end speed of 30m/s and wind....

As a designer I want to reduce the empty weight....

Design lift coefficient is determined by wing loading.

Determine wing loading for civil aircraft if lift-off speed is....

Equivalent skin friction coefficient can be used to provide initial....

Equivalent skin friction coefficient may include __

Aerodynamic Coefficients more Online Exam Quiz

Tail Geometry and Arrangement

Thrust Weight Ratio-1

Thrust Weight Ratio-2

Wing Geometry-1

Wing Geometry-2

Airbus A-320 Family of Aircraft's

Airbus A-330 Family of Aircraft's

Airbus A-350 Family of Aircraft's

Airbus A-380 Family of Aircraft's

Aircraft Cockpit