Technical Report Archive & Image Library (TRAIL) - 1,371 Matching Results

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Primary view of A 37,500 KW Power Reactor with Competitive Possibilities
Thompson, W. I. & Cohen, Karl
February 26, 1954
Primary view of Abernathyite, a New Uranium Mineral of the Metatorbernite Group
Thompson, M. E.; Ingram, Blanche & Gross, E. B.
August 1954
Primary view of The Absorption Spectra of Suspensions of Living Micro-Organism
Shibata, Kazuo, 1918-; Benson, Andrew A. & Calvin, Melvin, 1911-1997
June 1954
Primary view of Abstract for the Glasgow Meeting - "International Conference on Nuclear Physics": Gamma Transitions and the Shell Model
Goldhaber, M.
July 1954
Primary view of Acceleration of a Plasma by Time-Varying Magnetic Fields
Post, Richard F.
December 6, 1954
Primary view of Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics 3: effect of turbine stator adjustment
Rohlik, Harold E. & Rebeske, John J.
August 2, 1954
Primary view of Accepted Limit Values of Air Pollutants
Barkley, J. F.
May 1954
Primary view of Addendum to Report HW-30390:  Estimated Power Generation in MTR Slug Test Facility
Neumann, Hans, 1936-
September 20, 1954
Primary view of Additional Extraction and Ion Exchange Studies of Temple Mountain District Ores
Jones, J. Q. & Viklund, H. I.
July 30, 1954
Primary view of Additional Fatigue Tests on Effects of Design Details in 355-T6 Sand-Cast Aluminum Alloy
Eaton, I. D. & Youra, John A.
March 10, 1954
Primary view of Additional Results on the Static Longitudinal and Lateral Stability Characteristics of a 0.05-Scale Model of the Convair F2Y-1 Airplane at High Subsonic Speeds
Spreeman, Kenneth P. & Few, Albert G., Jr.
August 10, 1954
Primary view of Additional Static and Fatigue Tests of High-Strength Aluminum-Alloy Bolted Joints
Hartmann, E. C.; Holt, Marshall & Eaton, I. D.
July 1954
Primary view of The Aeolotropic Elastic Relations for Uranium Crystals
Merckx, K. R.
December 17, 1954
Primary view of Aerodynamic Characteristics at High and Low Subsonic Mach Numbers of the NACA 0012, 64₂-015, and 64₃-018 Airfoil Sections at Angles of Attack from -2 Degrees to 30 Degrees
Critzos, Chris C.
July 23, 1954
Primary view of Aerodynamic characteristics at Mach number of 2.01 of two cruciform missile configurations having 70 degree delta wings with length-diameter ratios of 14.8 and 17.7 with several canard controls
Spearman, M. Leroy & Robinson, Ross B.
August 30, 1954
Primary view of Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a 52.5 degree delta wing and a low, swept horizontal tail
Kehlet, Alan B.
March 29, 1954
Primary view of The aerodynamic characteristics at transonic speeds of a model with a 45 degree sweptback wing, including the effect of leading edge slats and a low horizontal tail
Runckel, Jack F. & Schmeer, James W.
April 5, 1954
Primary view of Aerodynamic characteristics including effects of wing fixes of a 1/20-scale model of the Convair F-102 airplane at transonic speeds
Osborne, Robert S. & Wornom, Dewey E.
March 18, 1954
Primary view of Aerodynamic Characteristics of a Circular Cylinder at Mach Number 6.86 and Angles of Attack Up to 90 Degrees
Penland, Jim A.
March 11, 1954
Primary view of Aerodynamic characteristics of a cruciform-wing missile with canard control surfaces and of some very small span wing-body missiles at a Mach number of 1.41
Spearman, M. Leroy & Robinson, Ross B.
April 12, 1954
Primary view of Aerodynamic characteristics of a full-span trailing-edge control on a 60 degree delta wing with and without a spoiler at Mach number 1.61
Lord, Douglas R. & Czarnecki, K. R.
March 10, 1954
Primary view of Aerodynamic characteristics of several flap-type trailing-edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01
Lord, Douglas R. & Czarnecki, K. R.
June 14, 1954
Primary view of Aerodynamic characteristics of several tip controls on a 60 degree wing at a Mach number of 1.61
Lord, Douglas R. & Czarnecki, K. R.
August 5, 1954
Primary view of Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)
Loftin, Laurence K., Jr.
August 1954
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