Question: What is the value of 'n' exponential in the fuel flow law for a high bypass ratio turbofan?

Options

A : 0.4

B : 0.5

C : 0.6

D : 0.7

Click to view Correct Answer

Previous || Next

Cruising Performance - Effect of Alternative Fuel Flow Laws more questions

ADD stands for __

Air data measurement does not consider the relative motion between....

The essential requirement of air data measurement is the state....

The formula for velocity of maximum specific air range is....

The formula for velocity of maximum specific endurance is ___

What is the velocity of maximum specific air range of....

What is the velocity of maximum specific endurance of the....

At which cases does descent of flow occur?

In cruise performance the fuel mass flow determines the rate....

In the case of gliders, the descent is calculated by....

Aerodynamic Relationships more Online Exam Quiz

Cruise Method 1 - 1

Cruise Method 1 - 2

Cruise Method 2

Cruise Method 3

Cruising Performance - Aircraft with Mixed Power Plants

Cruising Performance - Specific Air Range and Specific Endurance

Descent Performance in Aircraft Operations - 1

Descent Performance in Aircraft Operations - 2

Drag Force

Effect of WAT on Cruise Performance