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Primary view of Advanced Seminar in Reactor Physics
Smith, Nicholas M.
July 26, 1950
Primary view of Aerodynamic characteristics of NACA RM-10 missile in 8- by 6-foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98 1: presentation and analysis of pressure measurements (stabilizing fins removed)
Luidens, Roger W. & Simon, Paul C.
July 20, 1950
Primary view of Aerodynamic characteristics of NACA RM-10 missile in 8- by 6-foot supersonic wind tunnel at Mach numbers from 1.49 to 1.98 2: presentation and analysis of force measurements
Esenwein, Fred T.; Obery, Leonard J. & Schueller, Carl F.
July 21, 1950
Primary view of Altitude-Chamber Performance of British Roll-Royce Nene II Engine 4: Effect of Operational Variables on Temperature Distribution at Combustion-Chamber Outlets
Huntley, Sidney C.
July 3, 1950
Primary view of Altitude-Chamber Performance of British Rolls-Royce Nene II Engine 3 - 18.00-Inch-Diameter Jet Nozzle
Grey, Ralph E.; Brightwell, Virginia L. & Barson, Zelmar
July 10, 1950
Primary view of Analysis of a standard Pu solution by the control laboratories in 231 and 234-5 Buildings
Barton, G.B.
July 14, 1950
Primary view of An analysis of base pressure at supersonic velocities and comparison with experiment
Chapman, Dean R.
July 1950
Primary view of Analysis of Turbulent Free-Convection Boundary Layer on Flat Plate
Eckert, E. R. G. & Jackson, Thomas W.
July 12, 1950
Primary view of Analysis of V-g data obtained from several naval airplanes
Thornton, James O.
July 7, 1950
Primary view of Analytical and Experimental Investigation of Adiabatic Turbulent Flow in Smooth Tubes
Deissler, Robert G.
July 1950
Primary view of Analytical investigation of flow and heat transfer in coolant passages of free-convection liquid-cooled turbines
Eckert, E. R. G. & Jackson, Thomas W.
July 18, 1950
Primary view of Analytical Investigation of Turbines With Adjustable Stator Blades and Effect of These Turbines on Jet-Engine Performance
Silvern, David H. & Slivka, William R.
July 17, 1950
Primary view of Approximate aerodynamic influence coefficients for wings of arbitrary plan form in subsonic flow
Diederich, Franklin W.
July 1950
Primary view of An Approximate Crystal Structure for the Beta Phase of Uranium
Tucker, Charles W., Jr.
July 7, 1950
Primary view of Boundary-Layer Transition on a Cooled 20 Degree Cone at Mach Numbers of 1.5 and 2.0
Scherrer, Richard
July 1950
Primary view of Brookhaven National Laboratory, Annual Report, as of July 1, 1950. (Highlights)
Laboratory, Brookhaven National
July 1, 1950
Primary view of The calculation of downwash behind wings of arbitrary plan form at supersonic speeds
Martin, John C.
July 1950
Primary view of The calculation of modes and frequencies of a modified structure from those of the unmodified structure
Kruszewski, Edwin T. & Houbolt, John C.
July 1950
Primary view of Calculation of Transonic Flows Past Thin Airfoils by Integral Method
Perl, William
July 1950
Primary view of Chemical and physical properties vs degree of concentration of uranyl nitrate-nitric acid process streams of metal conversion plant
Clagett, F.
July 24, 1950
Primary view of CHEMISTRY DIVISION, SECTION C-I SUMMARY REPORT FOR APRIL, MAY, AND JUNE 1950
Osborne, D.W. ed.
July 27, 1950
Primary view of CHEMISTRY DIVISION, SECTION C-II SUMMARY REPORT FOR OCTOBER, NOVEMBER, AND DECEMBER 1949
Gilbreath, J.R. & Simpson, O.C. comps.
July 28, 1950
Primary view of COMPARATIVE BEHAVIOR OF A 1.8 ATOM % CHROMIUM-URANIUM ALLOY AND NORMAL URANIUM ON THERMAL CYCLING
White, D.W.
July 14, 1950
Primary view of Comparison of Model and Full-Scale Spin Test Results for 60 Airplane Designs
Berman, Theodore
July 1950
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