Question: If an aircraft is not designed properly then __
Options
A : it can experience excessive flow separation
B : it will have more lift
C : it will have less drag
D : it will have higher aerodynamic efficiency
Conceptual Sketch Sizing - Takeoff-Weight Calculation more questions
What is the first step to estimate the gross weight....
Which of the following is part of take-off weight estimation?
___ can be considered as one of the most powerful....
An aircraft has Crew and payload of 180kg. It has....
An aircraft has cruise range of 1500NM and SFC C....
Initial guess of gross weight will be same for every....
Keeping all other factors constant if only range of aircraft....
Poor wing fuselage will reduce lift loss.
To reduce fuselage wetted area we can ___
Total take-off gross weight depends on ___
Aerodynamic Coefficients more Online Exam Quiz
Conceptual Sketch Sizing - Empty-Weight Estimation
Conceptual Sketch Sizing - Fuel-Fraction Estimation-1
Conceptual Sketch Sizing - Fuel-Fraction Estimation-2
Conceptual Sketch Sizing - Takeoff-Weight Buildup
Configuration Layout - Aerodynamic Considerations-1
Configuration Layout - Aerodynamic Considerations-2
Configuration Layout - Conic Fuselage Development