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Primary view of 25 content of initial lots of Hanford UO{sub 3}
Work, J. B.
May 28, 1952
Primary view of 25 Process Assistance. For Period of May 2, 1955 to May 13, 1955
Culler, F L
May 23, 1955
Primary view of 215 MWD/Ton batch size limits and control in the Bismuth Phosphate Plant
Browne, W. G.
May 24, 1954
Primary view of Absorption Spectrum of Ferric Sulfate Complex
Katzin, L.I. & Gebert, E.
May 22, 1950
Primary view of The Absorption Spectrum of Hydrated Americium Chloride
Stover, Betsy Jones & Conway, John G.
May 2, 1952
Primary view of An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control
Gerus, Theodore F.; Powers, Albert G. & Heppler, Herbert J.
May 12, 1958
Primary view of An Acceleration Schedule Control for Accelerating a Turbojet Engine and Its Use With a Speed Control
Gerus, Theodore F.; Powers, Albert G. & Heppler, Herbert J.
May 12, 1958
Primary view of Accepted Limit Values of Air Pollutants
Barkley, J. F.
May 1954
Primary view of Adaptation of Combustion Principles to Aircraft Propulsion Volume 2: Combustion in Air-Breathing Jet Engines
Fuels and Combustion Research Division
May 2, 1956
Primary view of Adsorption of Xenon in an Activated Charcoal Column
Cantelow, H. P.
May 11, 1959
Primary view of AEC Hot Cells and Related Facilities
Fosdick, Ellery R.
May 1958
Primary view of AEC Hot Cells and Related Facilities
Fosdick, Ellery R.
May 1, 1958
Primary view of AEC Symposium on Particle-Fluid Mechanics
Thomas, D. G.
May 13, 1959
Primary view of Aerodynamic and Lateral-Control Characteristics of a 1/28-Scale Model of the Bell X-1 Airplane Wing-Fuselage Combination: Transonic-Bump Method
Lockwood, Vernard E.
May 5, 1950
Primary view of Aerodynamic Characteristics at a Mach Number of 1.25 of a 6-Percent-Thick Triangular Wing and 6- and 9-Percent-Thick Triangular Wings in Combination With a Fuselage: Wing Aspect Ratio 2.31, Biconvex Airfoil Sections
Hall, Albert W. & Morris, Garland J.
May 5, 1950
Primary view of Aerodynamic characteristics at Mach number 4.04 of a rectangular wing of aspect ratio 1.33 having a 6-percent-thick circular-arc profile and a 30-percent-chord full-span trailing-edge flap
Dunning, Robert W. & Ulmann, Edward F.
May 29, 1953
Primary view of The Aerodynamic Characteristics in Pitch of a 1/15-Scale Model of the Grumman F11F-1 Airplane at Mach Numbers of 1.41, 1.61, and 2.01, TED No. NACA DE 390
Driver, Cornelius
May 23, 1956
Primary view of Aerodynamic characteristics of a wing with unswept quarter-chord line, aspect ratio 4, taper ratio 0.6, and NACA 65A004 airfoil section: Transonic-bump method
Myers, Boyd C., II & Wiggins, James W.
May 8, 1950
Primary view of Aerodynamic Characteristics of Four Bodies of Revolution Showing Some Effects of Afterbody Shape and Fineness Ratio at Free-Stream Mach Numbers From 1.50 to 1.99
Cohen, Robert J.
May 22, 1951
Primary view of Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 degrees to 20 degrees at high subsonic speeds
Daley, Bernard N. & Lord, Douglas R.
May 1955
Primary view of Aerodynamic characteristics of two-plane, unswept tapered wings of aspect ratio 3 and 3-percent thickness from tests on a transonic bump
Emerson, Horace F. & Gale, Bernard M.
May 2, 1952
Primary view of The Aerodynamic Characteristics of Two Series of Lifting Bodies at Mach Number 6.86
Ridyard, Herbert W.
May 24, 1954
Primary view of Aerodynamic characteristics of various configurations of a model of a 45 degree swept-wing airplane at a Mach number of 2.01
Spearman, M. Leroy; Driver, Cornelius & Robinson, Ross B.
May 26, 1955
Primary view of Aerodynamic Characteristics of Wings Designed for Structural Improvement
Weil, Joseph & Polhamus, Edward C.
May 28, 1951
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