NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
A wall interference assessment/correction systemA Wall Signature method, the Hackett method, has been selected to be adapted for the 12-ft Wind Tunnel wall interference assessment/correction (WIAC) system in the present phase. This method uses limited measurements of the static pressure at the wall, in conjunction with the solid wall boundary condition, to determine the strength and distribution of singularities representing the test article. The singularities are used in turn for estimating wall interferences at the model location. The Wall Signature method will be formulated for application to the unique geometry of the 12-ft Tunnel. The development and implementation of a working prototype will be completed, delivered and documented with a software manual. The WIAC code will be validated by conducting numerically simulated experiments rather than actual wind tunnel experiments. The simulations will be used to generate both free-air and confined wind-tunnel flow fields for each of the test articles over a range of test configurations. Specifically, the pressure signature at the test section wall will be computed for the tunnel case to provide the simulated 'measured' data. These data will serve as the input for the WIAC method-Wall Signature method. The performance of the WIAC method then may be evaluated by comparing the corrected parameters with those for the free-air simulation. Each set of wind tunnel/test article numerical simulations provides data to validate the WIAC method. A numerical wind tunnel test simulation is initiated to validate the WIAC methods developed in the project. In the present reported period, the blockage correction has been developed and implemented for a rectangular tunnel as well as the 12-ft Pressure Tunnel. An improved wall interference assessment and correction method for three-dimensional wind tunnel testing is presented in the appendix.
Document ID
19930002722
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lo, Ching F.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Ulbrich, N.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Sickles, W. L.
(Calspan Corp. Arnold AFS, TN., United States)
Qian, Cathy X.
(Tennessee Univ. Space Inst. Tullahoma, TN, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1992
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NAS 1.26:190617
NASA-CR-190617
Accession Number
93N11910
Funding Number(s)
CONTRACT_GRANT: NAG2-733
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available