Conceptual Sketch Sizing - Fuel-Fraction Estimation-2 Online Exam Quiz
Conceptual Sketch Sizing - Fuel-Fraction Estimation-2 GK Quiz. Question and Answers related to Conceptual Sketch Sizing - Fuel-Fraction Estimation-2. MCQ (Multiple Choice Questions with answers about Conceptual Sketch Sizing - Fuel-Fraction Estimation-2
A fighter jet is flying with wing span of 90ft. If mean aerodynamic chord MAC is at 30ft from tip chord then, to design such wing which type of planform should I use?
Options
A : Delta
B : Rectangular
C : Square
D : Triangle
A jet aircraft is cruising at 12000ft. What will be the cruise leg (mission phase 'n') weight fraction?
Options
A : Wn/Wn-1 = e^{\left(-\frac{R*C}{V*\frac{L}{D}}\right)}
B : Wn/Wn+1 = e^{\left(-\frac{R*C}{V*\frac{L}{D}}\right)}
C : Wn/Wn-2 = e^{\left(-\frac{R*C}{V*\frac{L}{D}}\right)}
D : Wn/Wn-1 = e^{\left(-\frac{R*C}{V*\frac{L}{D}}\right)}
A prop-driven aircraft is cruising with 90% propeller efficiency. If, range of aircraft is 7*106 ft, C=1.38*10-7 s-1 and L/D = 14 then what will be the fuel weight fraction for the cruise?
Options
A : 0.9216
B : 0.9261
C : 0.9289
D : 0.9365
An Aircraft has gross weight of 10000lb. At the end of the mission segment it has weight fraction as 0.985. Determine fuel consumed for this mission.
Options
A : 150lb
B : 150kg
C : 60kg
D : 60lb
An unstable A/C configuration is a typical wing-aft tail body. IF MAC is 4m then, what would be the approximated location of the CG?
Options
A : 2m
B : 5m
C : 6m
D : 7m
As a designer, our task is to design wing layout such that the location of MAC from root chord or centre line is at 8ft. Find the appropriate value of the wingspan if wing is rectangular.
Options
A : 32ft
B : 50ft
C : 28m
D : 32m
Choose appropriate option for cruise mission leg weight fraction.
Options
A : Breguet endurance formula
B : Breguet range formula
C : Cruise invert method
D : Breguet approximation
Fuel consumption during cruise is affected by wetted area.
Options
A : TRUE
B : FALSE
C : -
D : -
How will you determine climb mission weight fraction?
Options
A : Climb Endurance
B : Loiter
C : Always constant
D : Cruise Speed
If all the other factors remain unchanged and only aerodynamic efficiency of the aircraft is doubled then, what will be the cruise segment fuel weight fraction?
Options
A : Will increase
B : Will decrease
C : Will remain same
D : Will be independent of aerodynamic efficiency
Aerodynamic Coefficients more Online Exam Quiz
Conceptual Sketch Sizing - Empty-Weight Estimation
Conceptual Sketch Sizing - Fuel-Fraction Estimation-1
Conceptual Sketch Sizing - Takeoff-Weight Buildup
Conceptual Sketch Sizing - Takeoff-Weight Calculation
Configuration Layout - Aerodynamic Considerations-1