The aspect ratio (AR) is given by __________(a) b/s(b) s/b(c) b^2/s(d) s^3/bI got this question in an online interview.My question comes from Pressure Coefficient in section Inviscid & Incompressible Flow of Aerodynamics

The aspect ratio (AR) is given by __________(a) b/s(b) s/b(c) b^2/s(d)

1.	The aspect ratio (AR) is given by __________(a) b/s(b) s/b(c) b^2/s(d) s^3/bI got this question in an online interview.My question comes from Pressure Coefficient in section Inviscid & Incompressible Flow of Aerodynamics
Answer» Correct choice is (c) b^2/s To ELABORATE: ASPECT RATIO (AR) is the ratio of span to the mean chord. It is given by the square of WING span divided by wing area. A long and narrow wing has a HIGH aspect ratio and vice versa. It is given by: AR = b^2/S where b is the wing span and S is the wing area.

Discussion

No Comment Found

Related InterviewSolutions

The combination of uniform flow and source flow gives ___________(a) flow past a cylinder(b) flow past a half body(c) flow past a full body(d) flow past a wedgeThis question was addressed to me in homework.This question is from Vortex Flow in portion Inviscid & Incompressible Flow of Aerodynamics
The amount of lift generated in the flow over a cylinder is __________(a) Infinity(b) Positive lift(c) Negative lift(d) No liftI got this question in examination.Question is from Nonlifting Flow over Cylinder topic in chapter Inviscid & Incompressible Flow of Aerodynamics
The stream function can be obtained by _______(a) sum of stream function of uniform flow and doublet flow(b) difference of stream function of uniform flow and doublet flow(c) sum of stream function of uniform flow and source flow(d) sum of stream function of uniform flow and sink flowI had been asked this question by my school teacher while I was bunking the class.My question is taken from Nonlifting Flow over Cylinder topic in chapter Inviscid & Incompressible Flow of Aerodynamics
The opposite case of the source flow is ___________(a) sink flow(b) doublet flow(c) source flow(d) source-sink flowThis question was posed to me in semester exam.This interesting question is from Source Flow topic in division Inviscid & Incompressible Flow of Aerodynamics
Consider a fixed point in a flow. The locus of all the point passed through this fixed point is called as _________(a) stream-line(b) pathline(c) streak lines(d) stream tubesI have been asked this question in class test.I would like to ask this question from Uniform Flow topic in section Inviscid & Incompressible Flow of Aerodynamics
What is the flow of velocity at the top of the cylinder?(a) Higher(b) Lower(c) Constant(d) Does not variesThis question was posed to me in unit test.This intriguing question comes from Lifting Flow over Cylinder topic in section Inviscid & Incompressible Flow of Aerodynamics
Which of the following is suitable for the jet of oil in an unbroken stream?(a) temperature(b) surface tension(c) capillarity(d) vapour pressureI have been asked this question in an interview.This intriguing question originated from Doublet Flow in division Inviscid & Incompressible Flow of Aerodynamics
In real life, zero drag is acceptable.(a) True(b) FalseI had been asked this question in an online interview.Query is from Nonlifting Flow over Cylinder topic in chapter Inviscid & Incompressible Flow of Aerodynamics
When the amount of fluid displaced is equal to weight of body, it is called as _______(a) metacentre(b) buoyancy(c) centre of buoyancy(d) centre of gravityI got this question in an interview.This key question is from Doublet Flow topic in division Inviscid & Incompressible Flow of Aerodynamics
Stream function is defined for ____________(a) 2D flow(b) 3D flow(c) 1D flow(d) multi-dimensional flowI had been asked this question in class test.This is a very interesting question from Source Flow topic in chapter Inviscid & Incompressible Flow of Aerodynamics

The aspect ratio (AR) is given by __________(a) b/s(b) s/b(c) b^2/s(d) s^3/bI got this question in an online interview.My question comes from Pressure Coefficient in section Inviscid & Incompressible Flow of Aerodynamics

Discussion

No Comment Found

Related InterviewSolutions

Reply to Comment