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Tantalum Determination
Author(s): Moshier, Ross W., Schwarberg, James E.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-300
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Secondary Electron Current From A Pulsed Electron Accelerator
Author(s): Evans, A. E., Breitenbecher, D. V., Cady, D. W., Antes, L. L.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1956-09
Report number: WADC TR 56-463
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Pohlhausen-type, Laminar, Incompressible Boundary Layer Solution
Author(s): Cramer, Kenneth R.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1956-12
Report number: WADC TR 56-569
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Ceramic Crucible For Melting Titanium
Author(s): Weber, Berthold C., Thompson, William M., Bielstein, Hans O., Schwartz, Murray A.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1956-09
Report number: WADC TR 56-372
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Two Dimensional Inflow Conditions For A Supersonic Compressor with Curved Blades
Author(s): Levine, Philip
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1956-05
Report number: WADC TR 55-387
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Systemization Of The Organic Reactions And Methods Of Formation Of The Common Explosives
Author(s): Cattorini, Joseph F., Williams, Theodore J.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1956-03
Report number: WADC TR 55-369
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Optical Measurements On A Stationary Turbine Grid And On Radial Flow Turbine
Author(s): Zobel, Theodor W., Doepp, Philip Von, Forster, Paul G.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1956-06
Report number: WADC TR 56-221
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Generalized Charts Of Detonation Parameters For Gaseous Mixtures
Author(s): Wolfson, Bernard T., Dunn, Robert G.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1956-03
Report number: WADC TR 54-585
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Quenching Of The Fluorescence Of B-naphthylamine By Oxygen And Nitric Oxide
Author(s): Dubois, Jean T.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1956-03
Report number: WADC TR 55-382

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