Surface and Flow Field Measurements on the FAITH Hill ModelA series of experimental tests, using both qualitative and quantitative techniques, were conducted to characterize both surface and off-surface flow characteristics of an axisymmetric, modified-cosine-shaped, wall-mounted hill named "FAITH" (Fundamental Aero Investigates The Hill). Two separate models were employed: a 6" high, 18" base diameter machined aluminum model that was used for wind tunnel tests and a smaller scale (2" high, 6" base diameter) sintered nylon version that was used in the water channel facility. Wind tunnel and water channel tests were conducted at mean test section speeds of 165 fps (Reynolds Number based on height = 500,000) and 0.1 fps (Reynolds Number of 1000), respectively. The ratio of model height to boundary later height was approximately 3 for both tests. Qualitative techniques that were employed to characterize the complex flow included surface oil flow visualization for the wind tunnel tests, and dye injection for the water channel tests. Quantitative techniques that were employed to characterize the flow included Cobra Probe to determine point-wise steady and unsteady 3D velocities, Particle Image Velocimetry (PIV) to determine 3D velocities and turbulence statistics along specified planes, Pressure Sensitive Paint (PSP) to determine mean surface pressures, and Fringe Imaging Skin Friction (FISF) to determine surface skin friction (magnitude and direction). This initial report summarizes the experimental set-up, techniques used, data acquired and describes some details of the dataset that is being constructed for use by other researchers, especially the CFD community. Subsequent reports will discuss the data and their interpretation in more detail
Document ID
20120006656
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Bell, James H. (NASA Ames Research Center Moffett Field, CA, United States)
Heineck, James T. (NASA Ames Research Center Moffett Field, CA, United States)
Zilliac, Gregory (NASA Ames Research Center Moffett Field, CA, United States)
Mehta, Rabindra D. (NASA Ames Research Center Moffett Field, CA, United States)
Long, Kurtis R. (Aerospace Computing, Inc. Mountain View, CA, United States)
Date Acquired
August 25, 2013
Publication Date
January 9, 2012
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
ARC-E-DAA-TN4556Report Number: ARC-E-DAA-TN4556
Meeting Information
Meeting: 50th AIAA Aerospace Sciences Meeting
Location: Nashville, TN
Country: United States
Start Date: January 9, 2012
End Date: January 12, 2012
Sponsors: American Inst. of Aeronautics and Astronautics