If thickness ratio t/c is less or equal to the 0.05 then, the wetted area is ____(a) Swet = 2.003*Sexposed(b) Swet = 2.003*4*Sexposed(c) Swet = 2/Sexposed(d) Swet = 2*SexposedI had been asked this question in an interview for job.My question is taken from Configuration Layout in section Configuration Layout and Loft of Aircraft Design

If thickness ratio t/c is less or equal to the 0.05 then, the wetted a

1.	If thickness ratio t/c is less or equal to the 0.05 then, the wetted area is ____(a) Swet = 2.003Sexposed(b) Swet = 2.0034Sexposed(c) Swet = 2/Sexposed(d) Swet = 2SexposedI had been asked this question in an interview for job.My question is taken from Configuration Layout in section Configuration Layout and Loft of Aircraft Design
Answer» The correct answer is (a) Swet = 2.003Sexposed Explanation: Thin BODY has thickness TENDS to NEGLIGIBLE. For a paper thin body WETTED area is twice of the EXPOSED or true planform area. However, for finite thickness of t <= 0.05c wetted area is approximated as Swet = 2.003*Sexposed.

Discussion

No Comment Found

Related InterviewSolutions

Production lofting and simple lofting both are same phenomena.(a) True(b) FalseI had been asked this question in an interview.I'd like to ask this question from Configuration Layout in section Configuration Layout and Loft of Aircraft Design
What do you mean by longitudinal control lines?(a) Smooth lines which controls overall shape of the conic cross-section(b) Lines which expands to vertical direction only(c) Lines which go in horizontal direction only(d) Line which can be expanded only in lateral directionThis question was posed to me during a job interview.Origin of the question is Configuration Layout topic in chapter Configuration Layout and Loft of Aircraft Design
Wing has planform area of 2m^2. If wing is paper thin then, find wetted area of the wing.(a) 4m^2(b) 10m^2(c) 5m^2(d) 20m^2The question was posed to me in final exam.Asked question is from Configuration Layout in chapter Configuration Layout and Loft of Aircraft Design
Following diagram shows _____________(a) Circle to square adapter(b) Triangle to circle adapter(c) Triangle to ellipse(d) Elliptic converterI have been asked this question in unit test.I would like to ask this question from Configuration Layout in chapter Configuration Layout and Loft of Aircraft Design
Define control station.(a) Original cross-section used for longitudinal control lines(b) Auxiliary lines(c) Conic shape with circle only(d) Elliptic contour onlyI have been asked this question by my school teacher while I was bunking the class.This intriguing question comes from Configuration Layout in portion Configuration Layout and Loft of Aircraft Design
A good sketch should include _______________(a) overall aerodynamic concepts, location of components etc(b) only lifting area(c) only drag area(d) only volumeThis question was addressed to me during an interview for a job.I need to ask this question from Configuration Layout topic in portion Configuration Layout and Loft of Aircraft Design
Which of the following is an advantage of conic lofting?(a) Availability of diverse curves(b) Availability of simple drag only(c) Availability of simple lift drag(d) Availability of lift and drag onlyI have been asked this question in a job interview.My question comes from Configuration Layout in portion Configuration Layout and Loft of Aircraft Design
An unstable A/C configuration is a typical wing-aft tail body. IF MAC is 4m then, what would be the approximated location of the CG?(a) 2m(b) 5m(c) 6m(d) 7mThe question was asked in final exam.This intriguing question comes from Configuration Layout in chapter Configuration Layout and Loft of Aircraft Design
Buttock-planes are used to __________(a) evaluate the smoothness of A/C fuselage(b) evaluate Lift(c) find lift curve(d) find lift curve slopeThe question was posed to me by my college director while I was bunking the class.Enquiry is from Configuration Layout topic in portion Configuration Layout and Loft of Aircraft Design
Following diagram represents _______________(a) cross-section development via longitudinal control lines(b) vertical plane(c) arbitrary body with circle profile only(d) body with elliptic profile onlyThis question was addressed to me in homework.The doubt is from Configuration Layout in chapter Configuration Layout and Loft of Aircraft Design

Discussion

No Comment Found

Related InterviewSolutions

Reply to Comment