Related InterviewSolutions

• The three critical flight dynamics parameters are?(a) Roll, pitch and yaw(b) Roll, pitch and jaw(c) Roll, play and yaw(d) Roll, play and jawI have been asked this question by my college director while I was bunking the class.This is a very interesting question from Flight Dynamics topic in division Flight Dynamics and Control of Aircraft Maintenance
• What happens if an aircraft yaws about its center of gravity?(a) A sideslip angle arises(b) Aircraft will crash(c) Aircraft will start descending(d) Angle of attack increasesThe question was posed to me in class test.This interesting question is from Flight Dynamics topic in division Flight Dynamics and Control of Aircraft Maintenance
• Which of the following gives the viscosity of flow?(a) Mach Number(b) Knudsen Number(c) Specific heat ratio(d) Reynolds NumberThis question was posed to me in class test.Question is taken from Flight Dynamics topic in division Flight Dynamics and Control of Aircraft Maintenance
• Which of the following is not an aerodynamic coefficient?(a) Pressure coefficient(b) Absolute temperature(c) Lift coefficient(d) Drag coefficientThe question was asked in class test.My doubt is from Flight Dynamics in chapter Flight Dynamics and Control of Aircraft Maintenance
• Control systems adjust the orientation of a vehicle about its __________(a) Pitch(b) Wheels(c) Centre of mass(d) Centre of gravityI got this question in an internship interview.Origin of the question is Flight Dynamics in section Flight Dynamics and Control of Aircraft Maintenance
• Which of the following is not true about yaw?(a) About the vertical body axis(b) Positive with the nose to starboard(c) Measured in Hertz(d) Type of rotationI got this question in an interview.This interesting question is from Flight Dynamics topic in portion Flight Dynamics and Control of Aircraft Maintenance
• Flight dynamics studies the efficiency of vehicles travelling through air.(a) True(b) FalseThis question was addressed to me in an interview for internship.This key question is from Flight Dynamics topic in section Flight Dynamics and Control of Aircraft Maintenance
• The equilibrium roll angle is known as __________(a) Roll angle(b) Angle of incidence(c) Zero bank angle(d) Angle of attackThe question was posed to me by my college director while I was bunking the class.This interesting question is from Flight Dynamics topic in portion Flight Dynamics and Control of Aircraft Maintenance
• Which is the most dominant force in spacecraft flight dynamics?(a) Gravitational force(b) Nuclear force(c) Air resistance force(d) Lift and dragI have been asked this question in unit test.This intriguing question comes from Flight Dynamics in chapter Flight Dynamics and Control of Aircraft Maintenance
• An aircraft adjusts the lift generated by the wings when it pitches nose up or down by adjusting the angle of attack.(a) True(b) FalseI have been asked this question in a national level competition.My enquiry is from Flight Dynamics in section Flight Dynamics and Control of Aircraft Maintenance