..30.2: apparently, bad advice to put screen ahead of honeycomb*
McKINNEY, M.O.; SHEIMAN, J.*
Evaluation of turbulence reduction devices for the Langley 8-ft transonic pressure tunnel*
NASA TM 81792*
1981. `
..30.2: unoriginal - recommmends screen after honeycomb. Some new data*
SCHEIMAN, J.; BROOKS, J.D.*
Comparison of experimental and theoretical turbulence reduction from screens, honeycomb and honeycomb-screen combinations*
J. Aircraft 18, 638 and NASA TP 1958*
1981. `
..30.2:model tests for Langley 8 -ft*
SCHEIMAN, J.*
Considerations for the installation of honeycomb and screens to reduce wind tunnel turbulence*
NASA TM 81868*
1981. `
..30.2: nearly-triangular tapered elbow with honeycomb at exit*
LONDON, A.L.; KLOPFER, G.; WOLF, S.*
Oblique flow headers for heat exchangers*
Stanford Univ. M.E. Dept. Report IL-97*
1988. `
..42.3,30.3: electrically-heated triangular honeycomb*
LIENHARD V, J.H.; VAN ATTA, C.W.*
Thermally stratifying a wind tunnel for buoyancy influenced flows*
Expts. in Fluids 7, 542*
1989. `
..30.2: tests in pipe downstream of a fan*
FARELL, C.; YOUSSEF, S.*
Experiments on turbulence management using screens and honeycombs*
J. Fluids Engg 118, 26*
1996. `
..06.0,30.2:  old Sheffield Univ. work*
AHMED, F.; LEE, B.E.*
The production of shear flow profiles in a wind tunnel by a shaped honeycomb technique*
J. Fluids Engg 119, 713*
1997. `
..19.1,44.2,30.2:  when spacing is small, turbulence becomes 2D.  Relevance to honeycombs*
GRAHAM, J.M.R.*
The effect of a two-dimensional cascade of thin streamwise plates on homogeneous turbulence*
J. Fluid Mech. 356, 125*
1998. `