WALL INTERFERENCE ASSESSMENT CORRECTION FOR TRANSONIC AIRFOIL DATA

被引：2

作者：

GREEN, LL

MINECK, RE

机构：

[1] NASA Langley Research Center, Hampton, VA

[2] CAB/FldMD

[3] TAB/AAD

来源：

JOURNAL OF AIRCRAFT | 1991年 / 28卷 / 11期

关键词：

D O I：

10.2514/3.46095

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Two sets of transonic airfoil data were obtained from the same model tested in both porous, planar-wall and solid, shaped-wall wind tunnels. The published data agree resonably well with each other but differ significantly from two-dimensional, free-air Navier-Stokes calculations for the same airfoil. An existing computational wall interference assessment/correction (WIAC) procedure was applied to the porous- and shaped-wall data sets. The WIAC corrections generally improve the correlation between the two data sets. Simultaneously, the WIAC corrections also generally improve the correlation between the data and the Navier-Stokes calculations.

引用

页码：774 / 780

页数：7

共 25 条

[1]

Seraudie A., Blanchard A., Briel J.F., Rapport D'essais Du Profil CAST 10 En Transition Declenchee Effectues Dans La Soufflerie Transsonique Cryogenique T2 En Presence De Parois Autoadaptables, (1985)

[2]

Brown D., Information for Users of the National Research Council's 5 Ft X 5 Ft Blowdown Wind Tunnel at the National Aeronautical Establishment, (1977)

[3]

Ohman L.E., The NAE High Reynolds Number 15 In. X 60 In. Two-Dimensional Test Facility. Part 1. General Information, (1970)

[4]

Chan Y.Y., Wind Tunnel Investigation of the CAST-10-2/DOA-2 12% Supercritical Airfoil Model, (1986)

[5]

Mokry M., Ohman L.H., Application of the Fast Fourier Transform to Two-Dimensional Wind Tunnel Wall Interference, Journal of Aircraft, 17, 6, pp. 402-408, (1980)

[6]

Ray E.J., Ladson C.L., Adcock J.B., Lawing P.L., Hall R.M., Review of the Design and Operating Characteristics of the 0.3-Meter Transonic Cryogenic Tunnel, (1979)

[7]

Mineck R.E., Hardware and Operating Features of the Adaptive Wall Test Section Hardware for the Langley 0.3-Meter Transonic Cryogenic Tunnel, (1989)

[8]

Mineck R.E., Wall Interference Tests of a CAST 10-2/DOA 2 Airfoil in an Adaptive-Wall Test Section, (1987)

[9]

Wolf S.W.D., Goodyer M.J., Predictive Wall Adjustment Strategy for Two-Dimensional Flexible Walled Adaptive Wind Tunnel-A Detailed Description of the First One Step Method, (1988)

[10]

Braslow A.L., Knox E.C., Simplified Method for Determination of Critical Height of Distributed Roughness Particles for Boundary Layer Transition at Mach Numbers from 0 to 5, (1958)

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