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1. A New Method of Determining Roughness Height For Low-Reynolds-Number Flows

open_access
Open Access
Author:
Morgan, Nicholas
Title:
A New Method of Determining Roughness Height For Low-Reynolds-Number Flows
Area of Honors:
Aerospace Engineering
Keywords:
airfoil
fixed transition
forced transition
low Reynolds
S407
E387
transition
Braslow
LSLT Wind Tunnel
Wind Tunnel
Low-Speed
File:
Download A_NEW_METHOD_OF_DETERMINING_ROUGHNESS_HEIGHT_FOR_LOW-REYNOLDS-NUMBER_FLOWS.pdf
Thesis Supervisors:
Mark David Maughmer, Thesis Supervisor
Robert Graham Melton, Thesis Honors Advisor
Amy Ruth Pritchett, Faculty Reader