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A Wall Correction Program Based on Classical Methods for the National Transonic Facility (Solid Wall or Slotted Wall) and the 14x22-Ft Subsonic Tunnel at NASA LaRCA Fortran subroutine CMWALL is described, which is an implementation of the collective information from classical methods-based wall corrections. These methods use established closed-form expressions which were developed based on simple linear potential-based methods. This is a simple and rapid tool to calculate corrections due to wall interference in the National Transonic Facility (Solid Wall or Slotted Wall) or the 14x22-Ft Subsonic Tunnel at NASA LaRC. It is designed to be easily implemented in the existing tunnel data reduction programs, either as real-time or post-point. It is however important to realize that the method is based on the simplifying assumptions of linearity, small model and attached flow. The computed results are thus to be viewed as first-cut estimates, to be refined further using more complex methods based on measured wall pressures (known as wall signature methods).
Document ID
20040191536
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Hemsch, Michael J.
(NASA Langley Research Center Hampton, VA, United States)
Iyer, Venkit
(Analytical Services and Materials, Inc. Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
October 1, 2004
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA/CR-2004-213261
Report Number: NASA/CR-2004-213261
Funding Number(s)
WORK_UNIT: WU 23-908-01-03
CONTRACT_GRANT: NNL04AA03B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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