The effect of TAS on airborne distance is half that of the ideal case.(a) True(b) FalseI have been asked this question during an online exam.This is a very interesting question from Effect on the Take-off Distances of Flight Variables topic in section Take-off and Landing Performance of Aircraft Performance

The effect of TAS on airborne distance is half that of the ideal case.

1.	The effect of TAS on airborne distance is half that of the ideal case.(a) True(b) FalseI have been asked this question during an online exam.This is a very interesting question from Effect on the Take-off Distances of Flight Variables topic in section Take-off and Landing Performance of Aircraft Performance
Answer» Correct answer is (a) True The explanation: The effect of TAS on airborne distance is half that of the ideal case. The airborne distance is given by SA=\(\FRAC{W}{(F_N-D)_{AV}}\BIG\{\frac{V_{2}^2-V_{LOF}^2}{2g}+35\Big\}\) where W is weight D is drag G is acceleration due to gravity V is velocity FN is normal force.

Discussion

No Comment Found

Related InterviewSolutions

The terminal phases consist of two parts.(a) True(b) FalseThe question was asked by my college director while I was bunking the class.Question is taken from Types of Take-off and Landing topic in portion Take-off and Landing Performance of Aircraft Performance
What are the terminal phases of the aircraft landing?(a) Take-off(b) Landing(c) Take-off and landing(d) En-routeThe question was posed to me by my college director while I was bunking the class.My question is from Types of Take-off and Landing in section Take-off and Landing Performance of Aircraft Performance
What is engine failure accountability?(a) management of landing during the engine failure(b) management of take-off during the engine failure(c) fuel management during the engine failure(d) thrust management during the engine failureThe question was posed to me in examination.My doubt stems from Types of Take-off and Landing topic in chapter Take-off and Landing Performance of Aircraft Performance
What is aspect ratio?(a) It is the ratio of square of wing span to wing area(b) It is the ratio of wing span to wing area(c) It is the ratio of square of wing area to wing span(d) It is the ratio of wing area to wing spanThe question was asked in my homework.My question comes from Types of Take-off and Landing in division Take-off and Landing Performance of Aircraft Performance
What is the formula of aspect ratio?(a) AS=\(\frac{b}{S}\)(b) AS=\(\frac{s}{b}\)(c) AS=\(\frac{S^2}{b}\)(d) AS=\(\frac{b^2}{S}\)The question was posed to me in class test.My doubt stems from Types of Take-off and Landing topic in chapter Take-off and Landing Performance of Aircraft Performance
Ski-jump take-off path is used by _______(a) military aircrafts(b) commercial aircrafts(c) passenger aircrafts(d) cargo aircraftsThis question was posed to me in class test.My doubt stems from Types of Take-off and Landing in portion Take-off and Landing Performance of Aircraft Performance
What is the aspect ratio when the wing is 10 feet long and 2 feet wide?(a) 5(b) 10(c) 50(d) 0.4I got this question in unit test.The query is from Types of Take-off and Landing topic in division Take-off and Landing Performance of Aircraft Performance
Which of the following are the correct type of take-off and landings?(a) reduced take-off and landing, short take-off and landing, vertical take-off and landing(b) short take-off and landing, vertical take-off and landing(c) convectional take-off and landing, reduced take-off and landing(d) convectional take-off and landing, reduced take-off and landing, short take-off and landing, vertical take-off and landing, short take-off and vertical landingI have been asked this question in my homework.Question is taken from Types of Take-off and Landing in division Take-off and Landing Performance of Aircraft Performance
The aircraft uses short take-off landing to reduce the take-off fuel demand.(a) True(b) FalseThe question was asked in an international level competition.This interesting question is from Types of Take-off and Landing in portion Take-off and Landing Performance of Aircraft Performance
High lift devices can be used to increase the maximum lift coefficient of an aircraft and reduce the lift off speed.(a) True(b) FalseThe question was posed to me at a job interview.Enquiry is from Types of Take-off and Landing topic in portion Take-off and Landing Performance of Aircraft Performance

Discussion

No Comment Found

Related InterviewSolutions

Reply to Comment