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A Simple Battery Operated Pirani Gauge Power Pack
Author(s): Turnbull, A. H.
Corporate Author(s): Atomic Energy Research Establishment
Date of Publication: 1950-01
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Wind Tunnel Tests of the Coanda Wing and Nozzle
Author(s): Young, D. W., Zonars, D.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1950-09
Report number: AF TR 6199
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Defrosting of High Performance Fighter Aircraft
Author(s): Knoernschild, E. M., Larson, L. V.
Corporate Author(s): Equipment Laboratory
Laboratory: Equipment Laboratory
Date of Publication: 1950-12-01
Report number: AF TR 6118
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Infra-Red Heating for Anti-Icing, De-Icing, and Defrosting of Aircraft Transparent Areas.
Author(s): Hasinger, S. H., Larson, L. V.
Corporate Author(s): Equipment Laboratory
Laboratory: Equipment Laboratory
Date of Publication: 1950-03-01
Report number: AF TR 6113
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Fundamental Characteristics of High Performance Hydraulic Systems
Author(s): Campbell, James E.
Corporate Author(s): North American Aviation, Inc.
Laboratory: Air Materiel Command
Date of Publication: 1950-06
Report number: AF TR 5997
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Jet Engine Fire Protection Program
Author(s): Klein, H. A.
Corporate Author(s): C-O-Two Fire Equipment Company
Date of Publication: 1950-02-01
Report number: AF TR 5870
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 12. On the Stresses and Deflection of Swept Thick-Walled Box Beams
Author(s): Fung, Y. C.
Corporate Author(s): Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 1950-09-01
Report number: AF TR 5761 Part 12
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 11. An Experimental Investigation of Stresses and Deflections in a Swept Thick-Walled Box Beam
Author(s): Williams, M. L., Hrebec, G. M.
Corporate Author(s): Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-09-01
Report number: AF TR 5761 Part 11
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 14. Errata and Revisions
Corporate Author(s): Guggenheim Aeronautical Laboratory
Laboratory: Air Materiel Command
Date of Publication: 1950-11-01
Report number: AF TR 5761 Part 14
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 4. Application of the Electric Analog Computer to the Elastic Plate Problem
Author(s): MacNeal, Richard H.
Corporate Author(s): Guggenheim Aeronautical Laboratory, California Institute of Technology
Laboratory: Air Materiel Command
Date of Publication: 1950-10-01
Report number: AF TR 5761 Part 4

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