In short, to solve this
problem fully, students had to:
- determine the
velocity field around the wing (this required quite involved numerical analysis
in the topic of potential flow)
- identify a region in
the flow field with flow speed and direction that met requirements stated or
implied in the problem
- use the potential
flow results to compute the drag force on the pitot tube to ensure stiffness and
strength were sufficient
- ensure the pitot tube
was sufficiently far away from the boundary layer (viscous flow effect region)
on the wing
This exercise tied
together the three major course elements to that point (potential flow, boundary
layers, and force coefficients) and introduced them to the next major element
(airfoils).
Hi
Jim,
Here is the info you
requested.
Pete
_________________________________________________________________
Dr.
Peter M. Ostafichuk
Instructor & Mech 2
Coordinator
Department of
Mechanical Engineering,
Mail: Room 2054-6250
Applied
Office: 087
CICSR Phone: 604-822-9614 Fax:
604-822-2403
Cell:
604-341-6434 Home: 604-738-6434
email: [log in to unmask]
_________________________________________________________________
From: Sibley,
Jim [mailto:[log in to unmask]]
Sent: October 18, 2005 2:51 PM
To: ostafich
Subject:
TBL
Hi
Would it be possible to get a copy
of your pitot tube exercise and the result
chart??
I would love to use it as an
example......in my next TBL workshop.
Thanks
Jim
_________________________________________________
Jim
Sibley
Manager
Centre for Instructional
Support
Faculty of Applied
Science
2208-6250 Applied
V6T
1Z4
Phone 604.822.9241
Fax
604.822.7006
Email [log in to unmask]
Web www.learning.apsc.ubc.ca
________________________________________________
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