This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Control-Surface Sizing”. 1. If a wing has span of 12m. Find the approximated length of the aileron of starboard wing. a) 2.4m b) 20m c) 15m d) 25m 2. High speed aircraft is affected by ____________ a) aileron reversal b) flap inversion … Read more
This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Geometry Sizing”. 1. The purpose of fuselage is ___________ a) to provide space for cargo and passenger b) to provide thrust c) to provide high lift d) to increase maximum lift 2. Fineness ratio of fuselage is ratio of _____________ a) fuselage … Read more
This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Fixed-Engine Sizing”. 1. Based on existing engine or based on new design, aircraft sizing can be done. a) True b) False 2. Existing engine used for sizing is called as __________ a) fixed engine b) unfixed engine c) differential engine d) rubber … Read more
This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Rubber-Engine Sizing”. 1. Process of determining the take-off gross weight and required fuel weight is called as ________ a) aircraft sizing b) aircraft Lofting c) aircraft drafting d) aircraft drawing 2. We can provide sizing based on new design only. a) True … Read more
This set of Aircraft Design online test focuses on “Selection of Thrust-Weight and Wing Loading”. 1. Low wing loading increases __________ a) weight and cost of aircraft b) weight only c) lofting d) drafting 2. For estimated value of the thrust loading, we got three different values of wing loading. As a designer typically which … Read more
This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Wing Loading”. 1. Wing loading is ratio of ___________ a) weight of the aircraft and the reference area of wing b) reference area of wing and power of engine c) lift to drag d) aerodynamic force thrust to drag 2. Wing loading … Read more
This set of Aircraft Design Questions and Answers for Experienced people focuses on “Thrust-Weight Ratio-2”. 1. Thrust loading is defined as ____________ a) ratio of thrust produced by an engine to the weight of the aircraft b) ratio of lift to thrust c) ratio of drag to thrust d) ratio of lift to weight 2. … Read more
This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Thrust Weight Ratio-1”. 1. A/C with higher thrust to weight ratio can accelerate more quickly. a) True b) False 2. Can we estimate thrust loading based on Wing loading? a) Yes b) No c) Both are same d) Are not related to … Read more
This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Tail Geometry and Arrangement”. 1. Typically tail provides ______ a) stability b) control c) stability and control d) accelerating force 2. Which tail profile is shown in below diagram? a) Cruciform tail b) T – tail c) H – tail d) Conventional … Read more
This set of Aircraft Design Questions and Answers focuses on “Wing Geometry-2”. 1. For high aspect ratio strength of the wing tip vortex is low. a) True b) False 2. If aspect ratio of wing is 8 and S=0.1m2 then, what will be the span of wing? a) 0.89m b) 0.89cm c) 0.89 d) 0.89inch … Read more
