NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Wind Tunnel Wall Interference Assessment and Correction, 1983Technical information focused upon emerging wall interference assessment/correction (WIAC) techniques applicable to transonic wind tunnels with conventional and passively or partially adapted walls is given. The possibility of improving the assessment and correction of data taken in conventional transonic wind tunnels by utilizing simultaneously obtained flow field data (generally taken near the walls) appears to offer a larger, nearer-term payoff than the fully adaptive wall concept. Development of WIAC procedures continues, and aspects related to validating the concept need to be addressed. Thus, the scope of wall interference topics discussed was somewhat limited.
Document ID
19850003703
Acquisition Source
Langley Research Center
Document Type
Conference Proceedings
Authors
Perry A. Newman (Langley Research Center Hampton, Virginia, United States)
Richard W. Barnwell (Langley Research Center Hampton, Virginia, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1983
Publication Information
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.55:2319
L-15812
NASA-CP-2319
Report Number: NAS 1.55:2319
Report Number: L-15812
Report Number: NASA-CP-2319
Meeting Information
Meeting: Wind Tunnel Wall Interference Assessment and Correction, 1983
Location: Hampton, VA
Country: US
Start Date: January 25, 1983
End Date: January 26, 1983
Sponsors: National Aeronautics and Space Administration
Accession Number
85N12011
Funding Number(s)
PROJECT: RTOP 505-31-53-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19850003704WorkWall interference measurements for three-dimensional models in transonic wind tunnels: Experimental difficulties19850003705WorkSurvey of ONERA activities on adaptive-wall applications and computation of residual corrections19850003706WorkWind tunnel wall interference in closed, ventilated and adaptive test sections19850003707WorkTwo- and three-dimensional model and wall data from a flexible-walled transonic test section19850003708WorkAssessment of lift- and blockage-induced wall interference in a three-dimensional adaptive-wall tunnel19850003709WorkA data base for three-dimensional all-interference code evaluation19850003710WorkInvestigations of flow field perturbations induced on slotted transonic-tunnel walls19850003711WorkEffect of upstream sidewall boundary layer removal on an airfoil test19850003712WorkPerformance of two transonic airfoil wind tunnels utilizing limited ventilation19850003713WorkExperiments suitable for wind tunnel wall interference assessment/correction19850003714WorkAsymptotic methods for wind tunnel wall corrections at transonic speed19850003715WorkEffect of boundary layers on solid walls in three-dimensional subsonic wind tunnels19850003716WorkNLR activities in the field of wind tunnel wall interference19850003717WorkProgress in wind tunnel wall interference assessment/correction procedures at the NAE19850003718WorkDevelopment in UK of a method for calculating tunnel wall corrections from flow measurements19850003719WorkTunnel constraint for a jet in crossflow19850003720WorkInterference from slotted walls19850003721WorkWind tunnel wall interference correction for aircraft models19850003722WorkAn inerference assessment approach for a three-dimensional slotted tunnel with sparse wall pressure data19850003723WorkDetermination of equivalent model geometry for tunnel wall interference assessment/correction19850003724WorkExperiences with a high-blockage model tested in the NASA Ames 12-foot pressure wind tunnel19850003725WorkReview of the advanced technology airfoil test program in the 0.3-meter transonic cryogenic tunnel19850003726WorkSome experience with Barnwell-Sewall type correction to two-dimensional airfoil data19850003727WorkAdaptation of a four-wall interference assessment/correction procedure for airfoil tests in the 0.3-m TCT19850003704WorkWall interference measurements for three-dimensional models in transonic wind tunnels: Experimental difficulties19850003705WorkSurvey of ONERA activities on adaptive-wall applications and computation of residual corrections19850003706WorkWind tunnel wall interference in closed, ventilated and adaptive test sections19850003707WorkTwo- and three-dimensional model and wall data from a flexible-walled transonic test section19850003708WorkAssessment of lift- and blockage-induced wall interference in a three-dimensional adaptive-wall tunnel19850003709WorkA data base for three-dimensional all-interference code evaluation19850003710WorkInvestigations of flow field perturbations induced on slotted transonic-tunnel walls19850003711WorkEffect of upstream sidewall boundary layer removal on an airfoil test19850003712WorkPerformance of two transonic airfoil wind tunnels utilizing limited ventilation19850003713WorkExperiments suitable for wind tunnel wall interference assessment/correction19850003714WorkAsymptotic methods for wind tunnel wall corrections at transonic speed19850003715WorkEffect of boundary layers on solid walls in three-dimensional subsonic wind tunnels19850003716WorkNLR activities in the field of wind tunnel wall interference19850003717WorkProgress in wind tunnel wall interference assessment/correction procedures at the NAE19850003718WorkDevelopment in UK of a method for calculating tunnel wall corrections from flow measurements19850003719WorkTunnel constraint for a jet in crossflow19850003720WorkInterference from slotted walls19850003721WorkWind tunnel wall interference correction for aircraft models19850003722WorkAn inerference assessment approach for a three-dimensional slotted tunnel with sparse wall pressure data19850003723WorkDetermination of equivalent model geometry for tunnel wall interference assessment/correction19850003724WorkExperiences with a high-blockage model tested in the NASA Ames 12-foot pressure wind tunnel19850003725WorkReview of the advanced technology airfoil test program in the 0.3-meter transonic cryogenic tunnel19850003726WorkSome experience with Barnwell-Sewall type correction to two-dimensional airfoil data19850003727WorkAdaptation of a four-wall interference assessment/correction procedure for airfoil tests in the 0.3-m TCT
No Preview Available