NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A skin friction gauge for impulsive flowsA new skin friction gauge has been designed for use in impulsive facilities. The gauge was tested in the T4 free piston shock tunnel, at the University of Queensland, using a 1.5 m long plate that formed one of the inner walls of a rectangular duct. The test gas was fair and the test section free stream flow had a stagnation enthalpy of 4.7 MJ/kg. Measurements were conducted in a laminar and turbulent boundary layer. The measurements compared well with laminar and turbulent analytical theory.
Document ID
19960001682
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Goyne, C. P.
(Queensland Univ. Brisbane, Australia)
Paull, A.
(Queensland Univ. Brisbane, Australia)
Stalker, R. J.
(Queensland Univ. Brisbane, Australia)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Publication Information
Publication: Shock Tunnel Studies of Scramjet Phenomena 1994
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 95-3152
Meeting Information
Meeting: AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Location: San Diego, CA
Country: United States
Start Date: July 10, 1995
End Date: July 12, 1995
Accession Number
96N11690
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available