36 reports
Flight Tests Of The F-84D Ejection Seat
Author(s): Hecht, K. F. Corporate Author: Aircraft Laboratory Date of Publication: 1950-12 Report Number: WADC TR 53-366
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Supervisor's Estimates of Educational Needs Among Subordinates
Author(s): Scates, Douglas E. Corporate Author: American Council on Education Date of Publication: 1950-09
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Developing an Objective Item Questionnaire to Assess the Market for Further Education Among Employed Adults
Author(s): Scates, Douglas E. Corporate Author: American Council on Education Date of Publication: 1950-08
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Phosphorography
Author(s): Dropkin, J. J. Corporate Author: Polytechnic Institute of Brooklyn Date of Publication: 1950-06-15
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Phosphorography
Author(s): Dropkin, J. J. Corporate Author: Polytechnic Institute of Brooklyn Date of Publication: 1950-09-15
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Experiments with a Differential Pirani Gauge Leak Detector
Author(s): Turnbull, A. H. Corporate Author: Atomic Energy Research Establishment Date of Publication: 1950-03
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The Principles of Leak Detection
Author(s): Turnbull, A. H. Corporate Author: Atomic Energy Research Establishment Date of Publication: 1950-03
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A Simple Battery Operated Pirani Gauge Power Pack
Author(s): Turnbull, A. H. Corporate Author: Atomic Energy Research Establishment Date of Publication: 1950-01
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 9. On the Stresses in Cantilever Plates of Arbitrary Planform and Variable Thickness (A Relaxation Procedure With Applications to the Swept Wing Problem)
Author(s): Fung, Y. C. Corporate Author: Guggenheim Aeronautical Laboratory Laboratory: Air Materiel Command Date of Publication: 1950-10-01 Report Number: AF TR 5761 Part 9
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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: 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 12. On the Stresses and Deflection of Swept Thick-Walled Box Beams
Author(s): Fung, Y. C. Corporate Author: 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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The Comparative Composite Validities of Batteries of "Short" Versus "Long" Tests
Author(s): Brokaw, Leland D. Corporate Author: Human Resources Research Center Laboratory: Directorate of Personnel Research Date of Publication: 1950-01 Report Number: HRRC RB 50-1
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Survey of Human Adjustment Problems in the Northern Latitudes
Author(s): Debons, Anthony Corporate Author: Arctic Aeromedical Laboratory Laboratory: Arctic Aeromedical Laboratory Date of Publication: 1950-05
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An Improved Type of Micro-Cell Carriage for the Hilger Spekker Photoelectric Absorptiometer Model H 560
Author(s): Sanders, C. Corporate Author: Atomic Energy Research Establishment Date of Publication: 1950-12
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Thermo-elastic Stress due to Aerodynamic Heating of Supersonic Wings. Part 1.
Author(s): Durham, Franklin P. Corporate Author: Colorado Engineering Experiment Station Date of Publication: 1950-07 Report Number: AF TR 6351 Part 1 AD Number: AD0002628
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Wind Tunnel Tests of the Coanda Wing and Nozzle
Author(s): Young, D. W. Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 1950-09 Report Number: AF TR 6199
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Thermoelastic Stresses In Beams
Author(s): Barrekette, Euval S. Corporate Author: Institute of Flight Structures; Columbia University Laboratory: Aircraft Laboratory Date of Publication: 1950-02 Report Number: WADC TR 59-178
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Fundamental Characteristics of High Performance Hydraulic Systems
Author(s): Campbell, James E. Corporate Author: North American Aviation, Inc. Laboratory: Air Materiel Command Date of Publication: 1950-06 Report Number: AF TR 5997
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Validity of the Airman Classificatiion Battery AC-1
Author(s): Gragg, Donald B. Corporate Author: Human Resources Research Center Laboratory: Directorate of Personnel Research Date of Publication: 1950-12 Report Number: HRRC RB 50-3
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 3. Experimental Investigation of the Effect of Sweep Upon the Stress and Deflection Distribution in Cantilever Plates of Constant Chord and Thickness
Author(s): DeGroff, Harold M. Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 1950-10-01 Report Number: AF TR 5761 Part 3
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The Application of The Hollow Cathode Ray Source to Spectrographic Analysis. Part 1. Apparatus
Author(s): Burks, F. T. Corporate Author: Atomic Energy Research Establishment Date of Publication: 1950-12
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity:
Author(s): Sechler, E. E. Corporate Author: Guggenheim Aeronautical Laboratory Laboratory: Air Materiel Command Date of Publication: 1950-12-01 Report Number: AF TR 5761 Part 13
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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 8. Some Experimental Data on the Deflection and Root Stresses in a Cantilever Triangular Plate of Constant Thickness With Varying Trailing Edge Sweep Angle
Author(s): Hrebec, G. M. Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 1950-11-01 Report Number: AF TR 5761 Part 8
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Neutron Diffusion at Large Distances from the Source
Author(s): Spinney, K. T. Corporate Author: Atomic Energy Research Establishment Date of Publication: 1950-01-12
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Jet Engine Fire Protection Program
Author(s): Klein, H. A. Corporate Author: 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 4. Application of the Electric Analog Computer to the Elastic Plate Problem
Author(s): MacNeal, Richard H. Corporate Author: 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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Theoretical and Experimental Effect of Sweep upon the Stress and Deflection Distribution in Aircraft Wings of High Solidity: Part 6. The Plate Problem for a Cantilever Sector of Uniform Thickness
Author(s): Williams, M. L. Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 1950-11-01 Report Number: AF TR 5761 Part 6
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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. Corporate Author: 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 7. An Experimental Investigation of the Stresses and Deflections in a Series of Cantilever Sectors of Uniform Thickness
Author(s): Williams, M. L. Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 1950-11-01 Report Number: AF TR 5761 Part 7
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Scientific and Professional Personnel: Examination Development and Selection Techniques: A Bibliography
Author(s): Rohrer, Margaret Corporate Author: University of California at Berkeley Date of Publication: 1950-07
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Continuous Fuel Sprays
Author(s): Dodge, R. A. Corporate Author: University of Michigan Date of Publication: 1950-07 Report Number: AF TR 6067 Part 1
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Titanium Carbide Base Cermets
Author(s): Shevlin, T. S. Corporate Author: Ohio State University Research Foundation Date of Publication: 1950-01 Report Number: AF TR 6089
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Infra-Red Heating for Anti-Icing, De-Icing, and Defrosting of Aircraft Transparent Areas.
Author(s): Hasinger, S. H. Corporate Author: Equipment Laboratory Laboratory: Equipment Laboratory Date of Publication: 1950-03-01 Report Number: AF TR 6113 AD Number: ADB954424
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Preparation and Use of Pile-Made Gamma Source for Industrial Radiography
Author(s): Eastwood, W. S. Corporate Author: Atomic Energy Research Establishment Date of Publication: 1950-12
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Analysis of Training Criteria for the Navigator-Bombardier
Author(s): Smith, Moncrieff H., Jr. Corporate Author: Human Resources Research Center Laboratory: Directorate of Bombardment Observer-Navigator Training Research Date of Publication: 1950-01 Report Number: HRRC RB 50-2
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Defrosting of High Performance Fighter Aircraft
Author(s): Knoernschild, E. M. Corporate Author: Equipment Laboratory Laboratory: Equipment Laboratory Date of Publication: 1950-12-01 Report Number: AF TR 6118 AD Number:
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