..30.2: vortex panel method plus BFA TBL model. 2D and axi.*
BORGER, G.G.*
The optimization of wind tunnel contractions for the subsonic range*
Ph.D. Thesis, Ruhr Univ., NASA-TT-F-16899*
1976. `
..30.3:3m x 2m,contraction ratio about 2 to 1 - see Watkins 1984*
HIRD, T.G.*
The design and construction of an industrial wind tunnel*
Royal Melbourne Inst. of Tech. Rept 114001R*
1979. `
..30.2,50.0: at large scale, "blocking effect" may even lead to decrease in intensity*
GOLDSTEIN, M.E.; DURBIN, P.A.*
The effect of finite turbulence spatial scale on the amplification of turbulence by a contracting stream*
J. Fluid Mech. 98, 473*
1980. `
..12.1,30.2:useful calcs and expts*
TULAPURKARA, E.G.; RAMJEE, V.*
Effect of contraction on screen-generated turbulence.*
Aero. J. 84, 290*
1980. `
..30.2: vel ratio rather than area ratio matters*
WINTER, K.G.; BOYD, C.*
A speculation on the influence of compressibility on the performance of a wind contraction cone*
RAE TM Aero 1896*
1981. `
..30.2,28.3: fiendish - ink jet in a tunnel contraction and annular at that*
HENDRIKS, F.*
Aerodynamics of ink jet printing*
J. Appl. Phot. Engg 6, no. 3, 83*
1981. `
..30.3:interesting but plausible flow angles at contraction exit*
MOREL, J.P.*
The ETW European transonic wind tunnel project - progress report*
ONERA T.P. 1981-121*
1981. `
..12.2,30.2:for tunnel contractions - vel ratio counts, approx*
BOYD, C.*
The influence of compressibility on the equations of the rapid distortion theory of turbulence*
RAE TR 81153*
1982. `
..30.2:parametric study of u and L effects*
MARION, A.; TAN-ATICHAT, J.; NAGIB, H.M.*
On the design of contractions and settling chambers for optimal turbulence manipulation in wind tunnels*
NASA CR 169847*
1983. `
..45.0,30.2: due to secondary flow in contraction*
MOKHTARI, S.; BRADSHAW, P.*
Longitudinal vortices in wind tunnel wall boundary layers*
Aero. J., Roy. Aero. Soc 87, 233*
1983. `
..30.2: field Laplace solution - for NMI large tunnel*
DOWNIE, J.H.; JORDINSON, R.; BARNES, F.H.*
On the design of three-dimensional wind tunnel contractions*
Aero J. 88, 287*
1984. `
..30.2: axi stream function calcs for analysis*
WATMUFF, J.H.*
Wind tunnel contraction design*
Ninth Australasian Fluid Mech Conf, Auckland New Zealand, p. 472*
1986. `
..30.2: can be large*
TAN-ATICHAT, J.; HARANDI, S.*
Effects of acoustic disturbances on measured flow characteristics through a contraction*
AIAA J. 25, 659*
1987. `
..30.2: nonuniformity less than predicted*
TULAPURKARA, E.G.; BHALLA, V.V.K.*
Experimental investigation of Morel's method for wind tunnel contractions*
J. Fluids Engg 110, 45*
1988. `
..30.2: VSAERO panel method plus Thwaites. BL part in AIAA J. 27, 372 (1989)*
BELL, J.H.; MEHTA, R.D.*
Contraction design for small low-speed wind tunnels*
NASA CR 177488, Contract NAS2-NCC-2-294*
1988. `
..30.2: VSAERO and Thwaites on centre plane*
BELL, J.H.; MEHTA, R.D.*
Boundary-layer predictions for small low-speed contractions (TN)*
AIAA J. 27, 372*
1989. `
..30.1:  potential-flow solutions to produce design rules*
SU, Y.*
Flow analysis and design of three-dimensional wind tunnel contractions*
AIAA J. 29, 1912*
1991. `
..30.2: adverse pressure gradients specified*
GIBBINGS, J.C.*
Incompressible flow in contracting ducts*
Aeronautical J., Roy Aero Soc. 97, 230*
1993. `
..30.2: axi. Morel calibrated by Euler calcs.*
FANG, F-M.*
A design method for contractions with square end sections*
J. Fluids Engg 119, 454*
1997. `
..30.2: matched power law profiles with prescribed continuous curvature. Constrained by separation margin (Green calcs.)*
RAMASESHAN, S.*
Optimization and development of superior profiles for two dimensional and axisymmetric contractions*
Ph.D. Thesis, Dept. of Aerospace Engg, Indian Institute of Science*
1997. `