Aircraft Design Questions and Answers – Flight Mechanics – Landing Analysis

This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Flight Mechanics – Landing Analysis”. 1. Following diagram represents ____________ a) typical landing analysis segments b) takeoff phase c) climbing d) takeoff ground roll 2. The segment marked by ‘?’ in following diagram is showing _____ a) approach b) climb c) takeoff … Read more

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Aircraft Design Questions and Answers – Flight Mechanics – Takeoff Analysis

This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Flight Mechanics – Takeoff Analysis”. 1. Following diagram represents ____________ a) segments of typical takeoff b) landing phase c) cruise to climb mission segment d) approach 2. Segment marked by ‘?’ in the diagram is called ________ a) typical ground roll b) … Read more

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Aircraft Design Questions and Answers – Flight Mechanics – Operating Envelope

This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Flight Mechanics – Operating Envelope”. 1. Falling diagram represents _________ a) operating envelope b) lift curve c) tire sizing d) empty weight diagram 2. The level flight envelope is determined by ________ a) stall limit lines and from zero specific power b) … Read more

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Aircraft Design Questions and Answers – Flight Mechanics – Energy-Maneuverability Methods

This set of Aircraft Design Question Paper focuses on “Flight Mechanics – Energy-Maneuverability Methods”. 1. Total energy of an aircraft is defined as ____________ a) sum of the potential and kinetic energy b) total kinetic energy only c) total potential energy only d) product of kinetic and potential energy 2. Total energy divided by the … Read more

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Aircraft Design Questions and Answers – Flight Mechanics – Gliding Flight-2

This set of Aircraft Design Assessment Questions and Answers focuses on “Flight Mechanics – Gliding Flight-2”. 1. Graphical representation of sink rate of sailplane is called ____________ a) typical speed polar b) drag polar wing c) lift curve of wing d) propulsion systems 2. Velocity for the best glide ratio is 100ft/s. Determine velocity for … Read more

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Aircraft Design Questions and Answers – Flight Mechanics – Gliding Flight-1

This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Flight Mechanics – Gliding Flight-1”. 1. For a typical gliding flight, thrust will be ________ a) zero b) equal to the lift c) always same as drag d) always same as weight 2. The tangent of glide angle is ________ a) equal … Read more

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Aircraft Design Questions and Answers – Flight Mechanics – Level Turning Flight

This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Flight Mechanics – Level Turning Flight”. 1. Corner speed is defined as __________ a) velocity for maximum instantaneous turn b) maximum lift velocity c) maximum aerodynamic efficiency d) minimum instantaneous turn speed 2. During level turning flight, lift of wing is canted. … Read more

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Aircraft Design Questions and Answers – Flight Mechanics – Steady Climbing and Descending Flight

This set of Aircraft Design written test Questions & Answers focuses on “Flight Mechanics – Steady Climbing and Descending Flight”. 1. What do you mean by rate of climb? a) Vertical velocity of an aircraft b) Lift of an aircraft c) Thrust required d) Drag polar 2. Ratio of vertical distance travelled to the horizontal … Read more

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Aircraft Design Questions and Answers – Flight Mechanics – Steady Level Flight-2

This set of Aircraft Design Questions and Answers for Campus interviews focuses on “Flight Mechanics – Steady Level Flight-2”. 1. Following diagram represents ____________ a) thrust required curve b) lift curve c) drag polar d) lift polar 2. Following diagram represents _________ a) lift induced thrust required b) zero lift thrust required c) drag polar … Read more

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Aircraft Design Questions and Answers – Flight Mechanics – Steady Level Flight-1

This set of Aircraft Design Multiple Choice Questions & Answers (MCQs) focuses on “Flight Mechanics – Steady Level Flight-1”. 1. Find climb angle of climb gradient is 0.6. Assume non accelerated flight. a) 31° b) 1.2 c) 4.5rad d) 9.94° 2. If my aircraft is in steady level flight and has thrust of 100 unit … Read more

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Manish Bhojasia - Founder & CTO at Sanfoundry
Manish Bhojasia, a technology veteran with 20+ years @ Cisco & Wipro, is Founder and CTO at Sanfoundry. He lives in Bangalore, and focuses on development of Linux Kernel, SAN Technologies, Advanced C, Data Structures & Alogrithms. Stay connected with him at LinkedIn.

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