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Primary view of A 704 Program for Computing Thermal Neutron Spectra in Infinite Homogenous Media
Nelkin, M S.
November 24, 1958
Primary view of Aerodynamic Characteristics of a 45 Degree Swept Wing Fighter Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Aerodynamic Characteristics of a 45 Degree Swept-Wing Fighter-Airplane Model and Aerodynamic Loads on Adjacent Stores and Missiles at Mach Numbers of 1.57, 1.87, 2.16, and 2.53
Oehman, Waldo I. & Turner, Kenneth L.
June 24, 1958
Primary view of Aerodynamic characteristics of a canard and an outboard-tail airplane model at a Mach number of 2.01
Spearman, M. Leroy & Robinson, Ross B.
March 24, 1958
Primary view of Aerodynamic characteristics of several jet-spoiler controls on a 45 degree sweptback wing at Mach numbers of 1.61 and 2.01
Lord, Douglas R.
June 24, 1958
Primary view of Behavior of Some Materials and Shapes in Supersonic Free Jets at Stagnation Temperatures Up to 4,210 Degrees F, and Descriptions of the Jets
Fields, E. M.; Hopko, Russell N.; Swain, Robert L. & Trout, Otto F., Jr.
February 24, 1958
Primary view of Calculation of the Lateral Stability of a Directly Coupled Tandem-Towed Fighter Airplane and Correlation with Experimental Data
Shanks, Robert E.
June 24, 1958
Primary view of DISSOCIATION OF H$sub 2$$sup +$ IONS BY ELECTRIC FIELDS
Hiskes, J.R. & Uretsky, J.L.
April 24, 1958
Primary view of EFFECT ON POWER COST OF SUBSTITUTING ALUMINUM FOR ZIRCONIUM FUEL CLADDING IN A BOILING WATER REACTOR
Albrecht, W.L.
July 24, 1958
Primary view of The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes
Nielsen, Jack N.
March 24, 1958
Primary view of The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes
Nielsen, Jack N.
March 24, 1958
Primary view of Effects of Leading-Edge Slat and Trailing-Edge Split Flap on the Aerodynamic Characteristics of a Wing-Fuselage Combination Having a Nearly Triangular Wing of Aspect Ratio 2.9 at Mach Numbers From 0.60 to 0.92
Demele, Fred A.
January 24, 1958
Primary view of Engineering Test Reactor Critical Facility Hazards Summary Report, Supplement I
deBoisblanc, D. R.; Burdick, Earl E. & DeBoer, T. K.
January 24, 1958
Primary view of ESTIMATE OF POTENTIAL FUEL REPROCESSING, REVISION NO. 22-PART A
Ullmann, J.W.
March 24, 1958
Primary view of An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers From 3.0 to 6.3
Gloria, Hermilo R.
June 24, 1958
Primary view of Feasibility of Nose-Cone Cooling by the Upstream Ejection of Solid Coolants at the Stagnation Point
Kinard, William H.
March 24, 1958
Primary view of Free-flight roll performance of a steady-flow jet-spoiler control on an 80 degree delta-wing missile between Mach numbers of 0.6 and 1.8
Schult, Eugene D.
January 24, 1958
Primary view of General Review of the Astron Thermonuclear Program
Christofilos, Nicholas C.
January 24, 1958
Primary view of A GENERATOR OF FAST-RISING LIGHT PULSES FOR PHOTOTUBE TESTING
Kerns, Q.A.; Kirsten, F.A. & Cox, G.C.
March 24, 1958
Primary view of Heat Transfer to 0 Degree and 75 Degree Swept Blunt Leading Edges in Free Flight at Mach Numbers From 1.90 to 3.07
O'Neal, Robert L. & Bond, Aleck C.
March 24, 1958
Primary view of High-speed landing loads measured on the Douglas X-3 research airplane
Marcy, William L.
February 24, 1958
Primary view of History and costs of waste storage at HAPO
Roberts, R. E.
March 24, 1958
Primary view of An Investigation of Supersonic Store Interference in the Vicinity of a 22 Degree Swept Wing Fuselage Configuration at Mach Numbers of 1.61 and 2.01
Geier, Douglas J.
February 24, 1958
Primary view of An investigation of supersonic store interference in the vicinity of a 22 degree swept-wing-fuselage configuration at Mach numbers of 1.61 and 2.01
Geier, Douglas J.
February 24, 1958
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