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Last edited by ImportBot
September 16, 2008 | History

Milton Lamb

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  • Cover of: Integration effects of D-shaped, underwing, aft-mounted, separate- flow, flow-through nacelles on a high-wing transport

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  • Cover of: Experimental and theoretical supersonic lateral-directional stability characteristics of a simplified wing-body configuration with a series of vertical-tail arrangements

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  • Cover of: Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle

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  • Cover of: 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

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  • Cover of: Stability and control characteristics of a monoplanar missile configuration with triform-tail-fin arrangements at mach numbers from 1.70 to 2.86

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  • Cover of: Integration effects of underwing forward- and rearward-mounted separate-flow, flow-through nacelles on a high-wing transport

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  • Cover of: Internal performance characteristics of thrust-vectored axisymmetric ejector nozzels

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  • Cover of: Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf

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History

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September 16, 2008 Created by ImportBot Imported from Miami University of Ohio MARC record