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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