Related InterviewSolutions

• Find the velocity for minimum thrust required at steady level flight if wing loading is 75N/m^2 and induced drag factor K is 0.0025. Consider CD0 as 0.02 and density as sea level.(a) 6.45m/s(b) 97m/s(c) 120m/s(d) 75m/sThe question was asked by my college professor while I was bunking the class.I need to ask this question from Flight Mechanics topic in section Performance and Flight Mechanics of Aircraft Design
• Following diagram represents ______________(a) drag polar(b) weight polar(c) thrust polar(d) lift curve slopeThis question was addressed to me in a national level competition.Question is taken from Flight Mechanics in chapter Performance and Flight Mechanics of Aircraft Design
• If static pressure of flow is 1200psf and operating Mach number is 1.19 then, determine the external flow dynamic pressure.(a) 1189.52 psf(b) 12.89 psf(c) 112 psf(d) 2587 psfI got this question in an interview for internship.This interesting question is from Flight Mechanics in section Performance and Flight Mechanics of Aircraft Design
• Which of the following is correct for a typical glider?(a) Drag D = W*cos (gamma)(b) Drag D = W*arcsine (gamma)(c) Drag D = W(d) Drag D = Thrust TI had been asked this question in a job interview.My doubt stems from Flight Mechanics in section Performance and Flight Mechanics of Aircraft Design
• Consider the vertical velocity of the aircraft is 10m/s and horizontal velocity is 12 m/s. Determine the value of climb gradient.(a) 0.833(b) 1.89(c) 8(d) 2.483This question was posed to me during a job interview.This intriguing question comes from Flight Mechanics topic in chapter Performance and Flight Mechanics of Aircraft Design
• All the gliders are unpowered.(a) True(b) FalseThe question was posed to me during a job interview.My question is from Flight Mechanics in chapter Performance and Flight Mechanics of Aircraft Design
• If Total energy of an aircraft is found to be 1200 unit and kinetic energy is 1100 unit then, determine the potential energy.(a) 100 unit(b) 213 unit(c) 456 unit(d) 500 unitThe question was asked during an interview for a job.My enquiry is from Flight Mechanics in section Performance and Flight Mechanics of Aircraft Design
• Consider a glider is descending from 2km altitude. If it covers range of 30km then, at which aerodynamic efficiency the glider was flying?(a) 15(b) 60(c) 12(d) 21This question was posed to me in quiz.This interesting question is from Flight Mechanics in section Performance and Flight Mechanics of Aircraft Design
• Variometer is used for _____________(a) informing pilot when glider is in lift(b) increase lift(c) thrust reversal(d) increase thrust producedThe question was asked in quiz.My doubt is from Flight Mechanics topic in chapter Performance and Flight Mechanics of Aircraft Design
• The level flight envelope is determined by ________(a) stall limit lines and from zero specific power(b) wing aileron size(c) spoilers area(d) tail areaI had been asked this question in an internship interview.Asked question is from Flight Mechanics topic in chapter Performance and Flight Mechanics of Aircraft Design