Question: Determine wing loading for civil aircraft if lift-off speed is 80m/s and maximum lift coefficient is 2.8.

Options

A : 9071.07

B : 9111

C : 911

D : 91

Click to view Correct Answer

Previous || Next

Wing Loading more questions

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

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

An aircraft is flying with wing loading of 50 and....

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

Design lift coefficient is determined by wing loading.

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

Equivalent skin friction coefficient may include __

For prop aircraft at maximum range what will be the....

Jet aircraft with CD=0.01+0.02CL2 is performing loiter. Find wing loading....

Low wing loading will provide ___

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