36 reports
Flight Tests Of The F-84D Ejection Seat
Author(s): K. F. Hecht Corporate Author: Aircraft Laboratory Date of Publication: 12/1/1950 Report Number: WADC TR 53-366
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Thermoelastic Stresses In Beams
Author(s): Euval S. Barrekette Corporate Author: Institute of Flight Structures; Columbia University Laboratory: Aircraft Laboratory Date of Publication: 2/1/1950 Report Number: WADC TR 59-178
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The Comparative Composite Validities of Batteries of "Short" Versus "Long" Tests
Author(s): Leland D. Brokaw Corporate Author: Human Resources Research Center Laboratory: Directorate of Personnel Research Date of Publication: 1/1/1950 Report Number: HRRC RB 50-1
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Analysis of Training Criteria for the Navigator-Bombardier
Author(s): Moncrieff H. Smith, Jr.; W. F. Long Corporate Author: Human Resources Research Center Laboratory: Directorate of Bombardment Observer-Navigator Training Research Date of Publication: 1/1/1950 Report Number: HRRC RB 50-2
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Validity of the Airman Classificatiion Battery AC-1
Author(s): Donald B. Gragg; Mary Agnes Gordon Corporate Author: Human Resources Research Center Laboratory: Directorate of Personnel Research Date of Publication: 12/1/1950 Report Number: HRRC RB 50-3
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Continuous Fuel Sprays
Author(s): R. A. Dodge; W. A. Haggerty; J. Louis York Corporate Author: University of Michigan Date of Publication: 7/1/1950 Report Number: AF TR 6067 Part 1
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Titanium Carbide Base Cermets
Author(s): T. S. Shevlin; C. C. McBride Corporate Author: Ohio State University Research Foundation Date of Publication: 1/1/1950 Report Number: AF TR 6089
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Thermo-elastic Stress due to Aerodynamic Heating of Supersonic Wings. Part 1.
Author(s): Franklin P. Durham Corporate Author: Colorado Engineering Experiment Station Date of Publication: 7/1/1950 Report Number: AF TR 6351 Part 1 AD Number: AD0002628
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Survey of Human Adjustment Problems in the Northern Latitudes
Author(s): Anthony Debons Corporate Author: Arctic Aeromedical Laboratory Laboratory: Arctic Aeromedical Laboratory Date of Publication: 5/1/1950
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Supervisor's Estimates of Educational Needs Among Subordinates
Author(s): Douglas E. Scates; Alice V. Yeomans Corporate Author: American Council on Education Date of Publication: 9/1/1950
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Developing an Objective Item Questionnaire to Assess the Market for Further Education Among Employed Adults
Author(s): Douglas E. Scates; Alice V. Yeomans Corporate Author: American Council on Education Date of Publication: 8/1/1950
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Scientific and Professional Personnel: Examination Development and Selection Techniques: A Bibliography
Author(s): Margaret Rohrer Corporate Author: University of California at Berkeley Date of Publication: 7/1/1950
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Phosphorography
Author(s): J. J. Dropkin Corporate Author: Polytechnic Institute of Brooklyn Date of Publication: 6/15/1950
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Phosphorography
Author(s): J. J. Dropkin Corporate Author: Polytechnic Institute of Brooklyn Date of Publication: 9/15/1950
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An Improved Type of Micro-Cell Carriage for the Hilger Spekker Photoelectric Absorptiometer Model H 560
Author(s): C. Sanders; A. W. Elson Corporate Author: Atomic Energy Research Establishment Date of Publication: 12/1/1950
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The Application of The Hollow Cathode Ray Source to Spectrographic Analysis. Part 1. Apparatus
Author(s): F. T. Burks Corporate Author: Atomic Energy Research Establishment Date of Publication: 12/1/1950
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Experiments with a Differential Pirani Gauge Leak Detector
Author(s): A. H. Turnbull Corporate Author: Atomic Energy Research Establishment Date of Publication: 3/1/1950
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The Principles of Leak Detection
Author(s): A. H. Turnbull Corporate Author: Atomic Energy Research Establishment Date of Publication: 3/1/1950
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Preparation and Use of Pile-Made Gamma Source for Industrial Radiography
Author(s): W. S. Eastwood Corporate Author: Atomic Energy Research Establishment Date of Publication: 12/1/1950
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Neutron Diffusion at Large Distances from the Source
Author(s): K. T. Spinney Corporate Author: Atomic Energy Research Establishment Date of Publication: 1/12/1950
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A Simple Battery Operated Pirani Gauge Power Pack
Author(s): A. H. Turnbull Corporate Author: Atomic Energy Research Establishment Date of Publication: 1/1/1950
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Wind Tunnel Tests of the Coanda Wing and Nozzle
Author(s): D. W. Young; D. Zonars Corporate Author: Aircraft Laboratory Laboratory: Aircraft Laboratory Date of Publication: 9/1/1950 Report Number: AF TR 6199
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Defrosting of High Performance Fighter Aircraft
Author(s): E. M. Knoernschild; L. V. Larson Corporate Author: Equipment Laboratory Laboratory: Equipment Laboratory Date of Publication: 12/1/1950 Report Number: AF TR 6118 AD Number:
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Infra-Red Heating for Anti-Icing, De-Icing, and Defrosting of Aircraft Transparent Areas.
Author(s): S. H. Hasinger; L. V. Larson Corporate Author: Equipment Laboratory Laboratory: Equipment Laboratory Date of Publication: 3/1/1950 Report Number: AF TR 6113 AD Number: ADB954424
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Fundamental Characteristics of High Performance Hydraulic Systems
Author(s): James E. Campbell Corporate Author: North American Aviation, Inc. Laboratory: Air Materiel Command Date of Publication: 6/1/1950 Report Number: AF TR 5997
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Jet Engine Fire Protection Program
Author(s): H. A. Klein Corporate Author: C-O-Two Fire Equipment Company Date of Publication: 2/1/1950 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): Y. C. Fung Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 9/1/1950 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): M. L. Williams; G. M. Hrebec Corporate Author: Guggenheim Aeronautical Laboratory Laboratory: Air Materiel Command Date of Publication: 9/1/1950 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: Guggenheim Aeronautical Laboratory Laboratory: Air Materiel Command Date of Publication: 11/1/1950 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): Richard H. MacNeal Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 10/1/1950 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): M. L. Williams Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 11/1/1950 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 3. Experimental Investigation of the Effect of Sweep Upon the Stress and Deflection Distribution in Cantilever Plates of Constant Chord and Thickness
Author(s): Harold M. DeGroff Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 10/1/1950 Report Number: AF TR 5761 Part 3
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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): M. L. Williams; J. Garrett; W. E. Henry Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 11/1/1950 Report Number: AF TR 5761 Part 7
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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): Y. C. Fung Corporate Author: Guggenheim Aeronautical Laboratory Laboratory: Air Materiel Command Date of Publication: 10/1/1950 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:
Author(s): E. E. Sechler; H. H. Dixon Corporate Author: Guggenheim Aeronautical Laboratory Laboratory: Air Materiel Command Date of Publication: 12/1/1950 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): G. M. Hrebec Corporate Author: Guggenheim Aeronautical Laboratory, California Institute of Technology Laboratory: Air Materiel Command Date of Publication: 11/1/1950 Report Number: AF TR 5761 Part 8
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