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44 items

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Design Charts For Axial-flow Compressors Having Constant Rotor work Distribution Over The Blade Span
Author(s): Hunter, Robert E.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1953-04
Report number: WADC TR 53-152
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Direct Synthesis Of Servomechanisms
Author(s): Budd, Frank W.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1953-06
Report number: WADC TR 53-420
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Electric Flowmeter (Thomas Principle)
Author(s): Penzig, F. G.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1954-07
Report number: WADC TR 54-352
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Merits Of Fuel Vaporization Blade Cooling In Super-sonic Turbojets with After Burning
Author(s): Samaras, Demetrios G.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1953-04
Report number: WADC TR 53-141
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Magneto-ionic Calculations
Author(s): Ross, Clarence, Fluke, Carl S.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1953-06
Report number: WADC TR 53-96
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An Analogue Series Computer
Author(s): Scherberg, Max G.
Corporate Author(s): Aeronautical Research Laboratory
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1954-08
Report number: WADC TR 54-174
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Five-channel Chronograph System For Detonation-wave Propagation Measurements
Author(s): Kissell, Kenneth E., Bollinger, Loren E., Dunn, Robert G.
Corporate Author(s): Aeronautical Research Laboratory
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1953-03
Report number: WADC TR 54-84
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Experimental Investigation Of The Shock Wave Pressure Characteristics Related to The Sonic Boom
Author(s): Daum, Fred L. , Smith, Norman
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1955-08
Report number: WADC TN 55-203
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Study OF The Effect Of Nonnormality On Sampling Distribution Of The Range
Author(s): Gephart, Landis G.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1955-03
Report number: WADC TR 55-128
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Analysis Of Traction Pumps
Author(s): Weinig, Friedrich S.
Corporate Author(s): Aeronautical Research Laboratory
Date of Publication: 1955-06
Report number: WADC TR 54-554

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