Organizational Unit:
Daniel Guggenheim School of Aerospace Engineering
Daniel Guggenheim School of Aerospace Engineering
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ItemAn experimental study for the prediction of pressure lag inherent in ballistic missile plumbing systems when subjected to continuous-type pressure functions(Georgia Institute of Technology, 1959-08) Hiers, Robert Smith
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ItemA study of the trajectories of a missile as a function of initial altitude, initial horizontal velocity and ballistic coefficient(Georgia Institute of Technology, 1959-05) Hutchinson, Herbert Alan
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ItemAn experimental study for the prediction of pressure lag inherent in ballistic missile plumbing systems when subjected to impulse-type pressure functions(Georgia Institute of Technology, 1959-05) Kowalsky, Bradley Dean
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ItemAn experimental study for the prediction of pressure lag inherent in ballistic missile plumbing systems, part I(Georgia Institute of Technology, 1958-12) Cremin, Joseph William
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ItemAn experimental investigation of pressure attenuation in typical missile plumbing systems subjected to shock wave inputs : effect of variation of receiver volume(Georgia Institute of Technology, 1958-12) Smith, Lester Robert
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ItemAn experimental investigation of pressure attenuation in typical missile plumbing systems subjected to shock wave inputs, part II(Georgia Institute of Technology, 1958-08) Kilburg, Richard Frank
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ItemAn experimental study for the prediction of pressure lag inherent in ballistic missile plumbing systems, part II(Georgia Institute of Technology, 1958-08) Ball, Karlheinz Otto Willi
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ItemAn experimental investigation of pressure attenuation in typical missile plumbing systems subjected to shock wave inputs, part I(Georgia Institute of Technology, 1958-08) DeJarnette, Fred Roark
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ItemA theoretical and experimental analysis of lengthwise pressure gradient for flow of air in small bore tubing considering the effect of elevated temperature(Georgia Institute of Technology, 1957-08) Laster, Marion Lynn
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ItemAn experimental investigation of air flow through insulated tubing as a function of approach temperature, pressure ratio, length, and diameter(Georgia Institute of Technology, 1957-08) Bradley, Richard Gordon