Cruise Method 3 Online Exam Quiz
Cruise Method 3 GK Quiz. Question and Answers related to Cruise Method 3. MCQ (Multiple Choice Questions with answers about Cruise Method 3
In Cruise method 3 endurance is more concentrated than distance travelled.
Options
A : TRUE
B : FALSE
C : -
D : -
In which of the following cases cruise method 3 is used?
Options
A : Commercial aircraft
B : Fighter aircraft
C : Military
D : Patrol and surveillance
The endurance of cruise method 3 is identical to that of cruise method 1.
Options
A : TRUE
B : FALSE
C : -
D : -
The range factor of cruise method 3 is identical to that of cruise method 1.
Options
A : TRUE
B : FALSE
C : -
D : -
The residual energy is converted into __
Options
A : power
B : thrust
C : lift
D : drag
What is a turboprop?
Options
A : It is a combination of turbojet and ramjet
B : It is a combination of turbojet and turbofan
C : It is a combination of turbojet and scramjet
D : It is a combination of turbojet and propeller engine
What is the range formula for mixed power-plant?
Options
A : R=Emax\big[?\frac{\eta}{C_P}+(1+?)\frac{uV_{md}}{C_T}\big]\big\{\frac{2u^2}{u^4-1}\big\}ln?
B : R=Emax\big[?\frac{\eta}{C_P}+(1-?)\frac{uV_{md}}{C_T}\big]\big\{\frac{2u^2}{u^4-1}\big\}ln?
C : R=Emax\big[?\frac{\eta}{C_P}+(1-?)\frac{uV_{md}}{C_T}\big]\big\{\frac{2u^2}{u^4+1}\big\}ln?
D : R=Emax\big[?\frac{\eta}{C_P}+(1+?)\frac{uV_{md}}{C_T}\big]\big\{\frac{2u^2}{u^4+1}\big\}ln?
What is the range of the power producing engine?
Options
A : RP=\big[\frac{\eta}{C_P}E_{max}\big]\big\{\frac{2u^2}{u^4+1}\big\}ln?
B : RP=\big[\frac{\eta}{C_P}E_{max}\big]\big\{\frac{2u^3}{u^4+1}\big\}ln?
C : RP=\big[\frac{\eta}{C_P}\big]\big\{\frac{2u^2}{u^4+1}\big\}ln?
D : RP=\big[\frac{V_{mdi}}{C_P}E_{max}\big]\big\{\frac{2u^3}{u^4+1}\big\}ln?
What is the range of thrust producing engine?
Options
A : RT=\big[\frac{V_{mdi}}{C_T}E_{max}\big]\big\{\frac{2u^4}{u^4+1}\big\}ln?
B : RT=\big[\frac{V_{mdi}}{C_T}\big]\big\{\frac{2u^3}{u^4+1}\big\}ln?
C : RT=\big[\frac{V_{mdi}}{C_T}E_{max}\big]\big\{\frac{2u^3}{u^4+1}\big\}ln?
D : RT=\big[\frac{V_{mdi}}{C_T}E_{max}\big]\big\{\frac{u^3}{u^4+1}\big\}ln?
Which of the following is a reason of disadvantage of cruise method 3?
Options
A : Increased mach number
B : Fuel saving
C : Increased time of flight
D : Increased weight of aircraft
Aerodynamic Relationships more Online Exam Quiz
Cruising Performance - Aircraft with Mixed Power Plants
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Cruising Performance - Specific Air Range and Specific Endurance