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Blimp Design-2003-Aeronautical Engineering And Sciences-Quiz Solution, Exercises of Aeronautical Engineering

This is solution to quiz Prof. Inesh Bachan took at Jiwaji University for for Aeronautical Engineering And Sciences. It includes: Proposed, Blimp, Design, Force, Shape, Similarly, Fluid, Solution, Parameters, Dimensional

Typology: Exercises

2011/2012

Uploaded on 07/20/2012

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Unified Engineering Fall 2003
Fluids Quiz 1 (QF5) Page 1/3
1. (30 %) A proposed winged blimp design flies at some angle of attack , and uses both
aerodynamic lift and aerostatic lift (buoyancy) to generate its total lift force L. The blimp
has a given shape, but its length c is as yet undecided.
c
a) In addition to the given and c, list all the remaining physical parameters which signifi-
cantly influence L.
g(L,�,c,...)=0
b) Determine a set of nondimensional parameters (or Pi products) which describe this situ-
ation.
c) Identify the nondimensional parameter which determines whether or not the aerodynamic
force is significant compared to the buoyancy force.
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Unified Engineering Fall 2003 Fluids Quiz 1 (QF5) Page 1/

  1. (30 %) A proposed winged blimp design flies at some angle of attack �, and uses both aerodynamic lift and aerostatic lift (buoyancy) to generate its total lift force L. The blimp has a given shape, but its length c is as yet undecided.

c

a) In addition to the given � and c, list all the remaining physical parameters which signifi cantly influence L. g(L, �, c,.. .) = 0

b) Determine a set of nondimensional parameters (or Pi products) which describe this situ ation.

c) Identify the nondimensional parameter which determines whether or not the aerodynamic force is significant compared to the buoyancy force.

Unified Engineering Fall 2003 Fluids Quiz 1 (QF5) Page 3/

  1. (30 %) A 2-D velocity field is given by

u(x, y) = x , v(x, y) = −y

a) Determine and sketch the streamline pattern.

b) Determine the circulation around the unit-square curve shown (Note: This is curve is not a streamline of this flow)

y

1

1

x