Return to search

Floating head skin friction gage measurements in supersonic flows

Two floating head skin friction gages have been designed and tested to directly measure the skin friction coefficient for the undefined flow in a SCRAM-jet engine. The skin friction gage designs contain a floating head that is supported by ball bearings which allow it to move in any horizontal direction and restrain it from any vertical motion. The shearing force caused by the supersonic flow deflects the floating head parallel to the flow direction. Strain gages mounted across a small gap between the bottom of the floating element and the bottom clamp provide the restoring force on the floating head. These strain gages also measure the floating head deflection caused by the flow shearing force.

The steel model design was built and tested to determine the feasibility of the design concept. The results from the supersonic wind tunnel at Mach 2.4 were reasonable but the steel model was unable to correctly respond to the short-duration flow of the shock tunnel. A skin friction gage made of a machinable ceramic called Macor was then designed to increase the resonant natural frequency (3600 Hz) and the insulating properties of the gage. Consequently, the Macor model floating head design is capable of measuring the skin friction coefficient in short duration, high enthalpy supersonic flows as well as long duration supersonic flows. The Macor model design yielded skin friction coefficient values near the expected value of 0.0014 when placed in a supersonic tunnel at both Mach 2.4 and Mach 3.0 and in a Mach 3.0 shock tunnel. / Master of Science

Identiferoai:union.ndltd.org:VTETD/oai:vtechworks.lib.vt.edu:10919/43485
Date30 June 2009
CreatorsLattimer, Brian Y.
ContributorsMechanical Engineering
PublisherVirginia Tech
Source SetsVirginia Tech Theses and Dissertation
LanguageEnglish
Detected LanguageEnglish
TypeThesis, Text
Formatxvii, 142 leaves, BTD, application/pdf, application/pdf
RightsIn Copyright, http://rightsstatements.org/vocab/InC/1.0/
RelationOCLC# 29250905, LD5655.V855_1993.L377.pdf

Page generated in 0.0022 seconds