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A fluctuating surface pressure test technique utilizing Mach number sweeps at transonic speedsA multichannel on-line RMS data acquisition and reduction system has been developed using commercial RMS computing modules and a programmable calculator. Details of this system, which has the capability of acquiring 96 channels of RMS data and computing and printing desired parameters in near real-time, are presented. In addition, raw data can be recorded at a much higher rate for computation and printing later. Results are presented showing the benefits of this system in 'sweep' tests where one parameter such as Mach number or angle of attack is slowly varied with time.
Document ID
19740052648
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hanly, R. D.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
July 1, 1974
Subject Category
Instrumentation And Photography
Report/Patent Number
AIAA PAPER 74-634
Meeting Information
Meeting: Aerodynamic Testing Conference
Location: Bethesda, MD
Start Date: July 8, 1974
End Date: July 10, 1974
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A35398
Distribution Limits
Public
Copyright
Other

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