Milton Lamb

William Milton Lamb (14 July 1909 – 21 June 2006) was an Australian rules footballer who played with Geelong in the Victorian Football League (VFL). Provided by Wikipedia
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  1. 1
    Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport

    Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport by Lamb, Milton

    Published 1986
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  2. 2
    Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle

    Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle by Lamb, Milton

    Published 1985
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  3. 3
    Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle

    Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle by Lamb, Milton

    Published 1985
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  4. 4
    Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport

    Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport by Lamb, Milton

    Published 1987
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  5. 5
    Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0̊ to 180̊ /

    Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0̊ to 180̊ / by Lamb, Milton

    Published 1976
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  6. 6
    A study of panel loads and centers of pressure of three different cruciform aft-tail control surfaces of a wingless missile from March 1.60 to 3.70 /

    A study of panel loads and centers of pressure of three different cruciform aft-tail control surfaces of a wingless missile from March 1.60 to 3.70 / by Lamb, Milton

    Published 1980
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  7. 7
    Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 /

    Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86 / by Lamb, Milton

    Published 1981
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  8. 8
    Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements /

    Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements / by Lamb, Milton

    Published 1981
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  9. 9
    Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels

    Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels by Lamb, Milton

    Published 1995
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  10. 10
    Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities /

    Sweep effect on the drag of rows of perpendicular circular cylinders in a laminar boundary layer at supersonic free-stream velocities / by Lamb, Milton

    Published 1974
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  11. 11
    Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf

    Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf by Lamb, Milton

    Published 1996
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  12. 12
    Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 /

    Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 / by Carson, George T., Lamb, Milton

    Published 1988
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  13. 13
    Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 /

    Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 / by Stallings, Robert L., Lamb, Milton

    Published 1980
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  14. 14
    Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /

    Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport / by Lamb, Milton, Carlson, John R., Pendergraft, Odis C.

    Published 1987
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  15. 15
    Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf /

    Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf / by Lamb, Milton, Taylor, John G., Frassinelli, Mark C.

    Published 1996
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  16. 16
    Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55̊ swept delta wing at supersonic speeds /

    Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55̊ swept delta wing at supersonic speeds / by Stallings, Robert L.

    Published 1977
    Other Authors: “…Lamb, Milton…”
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  17. 17
    Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

    Pressure distributions on three different cruciform aft-tail control surfaces of a wingless missile at mach 1.60, 2.36, and 3.70 /

    Published 1979
    Other Authors: “…Lamb, Milton…”
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  18. 18
    Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3

    Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 by Stallings, Robert L.

    Published 1980
    Other Authors: “…Lamb, Milton…”
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  19. 19
    Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds /

    Wing-alone aerodynamic characteristics for high angles of attack at supersonic speeds / by Stallings, Robert L.

    Published 1981
    Other Authors: “…Lamb, Milton…”
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  20. 20
    Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50 /

    Body-surface pressure data on two monoplane-wing missile configurations with elliptical cross sections at Mach 2.50 / by Allen, Jerry M.

    Published 1983
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