Pivot point is defined as?(a) The point at which the landing gear leg is attached to the aircraft(b) The point at which thrust forces is acting(c) The point with maximum lift to drag(d) CG of only quadric cycle gearI had been asked this question in an online interview.The query is from Gear-Retraction Geometry in portion Landing Gear and Subsystems of Aircraft Design

Pivot point is defined as?(a) The point at which the landing gear leg

1.	Pivot point is defined as?(a) The point at which the landing gear leg is attached to the aircraft(b) The point at which thrust forces is acting(c) The point with maximum lift to drag(d) CG of only quadric cycle gearI had been asked this question in an online interview.The query is from Gear-Retraction Geometry in portion Landing Gear and Subsystems of Aircraft Design
Answer» Right choice is (a) The point at which the LANDING gear LEG is attached to the aircraft For EXPLANATION: The point at which landing gear or undercarriage leg is attached to the aircraft is known as pivot point. This pivot point can be located anywhere ALONG the normal bisector to the line joining the up and down wheel positions. Lift to drag will be maximum at thrust required minimum.

Discussion

No Comment Found

Related InterviewSolutions

Following diagram represents _________(a) multi bogey(b) pusher prop(c) wing(d) bicycleI have been asked this question in an online quiz.My question comes from Landing Gear Arrangements in portion Landing Gear and Subsystems of Aircraft Design
Following diagram represents ____________(a) bicycle(b) tricycle(c) tail dragger(d) quadrupleI have been asked this question by my school principal while I was bunking the class.This is a very interesting question from Landing Gear Arrangements topic in division Landing Gear and Subsystems of Aircraft Design
What is the location of main wheel in tricycle gear?(a) After CG of the aircraft(b) At CG(c) Before CG(d) At noseThis question was posed to me during an interview for a job.The above asked question is from Landing Gear Arrangements in section Landing Gear and Subsystems of Aircraft Design
Let’s consider we want to design a seaplane which has the deadrise angle of 10° then, what should be the stall speed in in miles per hour?(a) 40mph(b) 89mph(c) 10mph(d) 21.9mphThe question was asked during a job interview.My doubt is from Landing Gear and Subsystems in portion Landing Gear and Subsystems of Aircraft Design
Which of the following is correct?(a) Sway brace is typically used for main landing gear(b) Lift is always same as weight(c) Lift opposes the aircraft forward motion(d) Drag is propulsive force produced by landing gear to accelerate an aircraftThe question was asked in semester exam.My question is based upon Gear-Retraction Geometry in section Landing Gear and Subsystems of Aircraft Design
Following diagram represents _________(a) tail dragger(b) bicycle(c) tricycle(d) single mainThe question was asked in an interview.Query is from Landing Gear Arrangements in section Landing Gear and Subsystems of Aircraft Design
We should always use tail dragger arrangement for every aircraft.(a) True(b) FalseThis question was addressed to me in semester exam.My question is based upon Landing Gear Arrangements topic in chapter Landing Gear and Subsystems of Aircraft Design
Which of the following is correct?(a) Landing gear is also termed as undercarriage(b) Tail dragger arrangement is most stable(c) Lift coefficient is same as weight always(d) Lift to thrust is called thrust loadingI have been asked this question during an interview for a job.My question is based upon Landing Gear Arrangements topic in division Landing Gear and Subsystems of Aircraft Design
Following diagram represents ______(a) gear retraction geometry(b) in cockpit(c) gear load chart(d) drag polarThis question was addressed to me during an online exam.Origin of the question is Gear-Retraction Geometry in section Landing Gear and Subsystems of Aircraft Design
Which of the following is correct?(a) Solid spring shock absorber is heavier than the other types(b) Lift to drag ratio is always unity(c) Weight at takeoff is same as weight at landing(d) Thrust is same as drag alwaysThis question was addressed to me during an interview.Origin of the question is Landing Gear in chapter Landing Gear and Subsystems of Aircraft Design

Discussion

No Comment Found

Related InterviewSolutions

Reply to Comment