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
    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

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981
    Format: Government Document Book


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  2. 2
    Heat-transfer distributions on a 0.013-scale shuttle solid rocket booster at Mach 3.70 and angles of attack from 0 ̊to 180 ̊

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

    Washington : Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service, 1976
    Format: Government Document Book


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  3. 3
    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

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981
    Format: Government Document Book


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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

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1987
    Format: Government Document Book


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  5. 5
    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

    Hampton, Va. : Springfield, VA :; Hampton, Va. : Springfield, VA : National Aeronautics and Space Administration, Langley Research Center ; National Technical Information Service, distributor, 1996
    Format: Government Document Book


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  6. 6
    Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels

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

    Hampton, Va. : [Springfield, Va.] : National Aeronautics and Space Administration, Langley Research Center ; [National Technical Information Service, distributor], 1995
    Format: Government Document Book


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  7. 7
    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

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1987
    Format: Government Document Book


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  8. 8
    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

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [For sale by the National Technical Information Service], 1980
    Format: Government Document Book


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  9. 9
    Effects of roughness size on the position of boundary-layer transition and on the aerodynamic characteristics of a 55 ̊swept delta wing at supersonic speeds

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

    [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1977
    Other Authors: “…Lamb, Milton…”
    Format: Government Document Book


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  10. 10
    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.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1981
    Other Authors: “…Lamb, Milton…”
    Format: Government Document Book


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  11. 11
    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.

    Washington, D.C. : [Springfield, Va.] :; Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service],; National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1980
    Other Authors: “…Lamb, Milton…”
    Format: Government Document Book


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  12. 12
    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

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1979
    Other Authors: “…Lamb, Milton…”
    Format: Government Document Book


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  13. 13
    Integration effects of pylon geometry on a high-wing transport plane

    Integration effects of pylon geometry on a high-wing transport plane by Carlson, John R.

    [Washington, DC] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; For sale by the National Technical Information Service], 1989
    Other Authors: “…Lamb, Milton…”
    Format: Government Document Book


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  14. 14
    Integration effects of pylon geometry on a high-wing transport plane

    Integration effects of pylon geometry on a high-wing transport plane by Carlson, John R.

    [Washington, DC] : [Springfield, Va.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [For sale by the National Technical Information Service], 1989
    Other Authors: “…Lamb, Milton…”
    Format: Government Document Book


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  15. 15
    Black contributors to American culture.

    Black contributors to American culture. by Ford, Helen

    Other Authors: “…Lamb, Milton C.…”
    Format: Audio


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  16. 16
    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.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1983
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    Format: Government Document Book


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  17. 17
    Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards

    Aerodynamic characteristics at Mach numbers of 1.5, 1.8, and 2.0 of a blended wing-body configuration with and without integral canards by Robins, A. Warner

    [Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Office, 1979
    Other Authors: “…Lamb, Milton…”
    Format: Government Document Book


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  18. 18
    Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds

    Effect of Reynolds number on stability characteristics of a cruciform wing-body at supersonic speeds by Stallings, Robert L.

    Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [for sale by the National Technical Information Service], 1980
    Other Authors: “…Lamb, Milton…”
    Format: Government Document Book


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