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Primary view of Analytical Chemistry Division Semiannual Progress Report For Period Ending April 20,1955
Kelley, M. T.; Susano, C. D. & Raaen, H. P.
May 6, 1955
Primary view of Corrosion in 650 F Degassed Water of Uranium-Molybdenum Alloys Containing Impurity Additions
Cawthorne, Edward W.; Berry, Warren E., 1922-; Reynolds, James E.; Jaffee, Robert Isaac, 1917- & Peoples, Robert S.
October 6, 1955
Primary view of Effects of Wing-Mounted Tank-Type Stores on the Low Lift Buffeting and Drag of a Swept-Wing Airplane Configuration Between Mach Numbers of 0.8 and 1.3
Mason, Homer P.
October 6, 1955
Primary view of Experimental Static Aerodynamic Forces and Moments at Low Speed on a Canard Missle During Simulated Launching From the Midsemispan and Wing-Tip Locations of a 45 Degree Sweptback Wing-Fuselage Combination
Alford, William J., Jr.
April 6, 1955
Primary view of Flight and Preflight Tests of a Ram Jet Burning Magnesium Slurry Fuel and Utilizing a Solid-Propellant Gas Generator for Fuel Expulsion
Bartlett, Walter A., Jr. & Hagginbothom, William K., Jr.
April 6, 1955
Primary view of Flight Measurements of the Dynamic Lateral and Longitudinal Stability of the Bell X-5 Research Airplane at 58.7 Degrees Sweepback
Videan, Edward N.
October 6, 1955
Primary view of Flight Tests of a Delta-Wing Vertically Rising Airplane Model Powered by a Ducted Fan
Lovell, Powell M., Jr.
April 6, 1955
Primary view of Free-flight investigation to obtain drag-at-lift and stability data for a 60 degree delta-wing-body configuration over a Mach number range of 1.3 to 1.6
Welsh, Clement J.
October 6, 1955
Primary view of Free-Spinning-Tunnel Investigation of a 0.034-Scale Model of the Production Version of the Chance Vought F7U-3 Airplane, TED No. NACA AD 3103
Klinar, Walter J. & Healy, Frederick M.
July 6, 1955
Primary view of Homogenous Reactor Project Quarterly Progress Report For Period Ending January 31, 1955
McDuffie, H. F. & Kelly, D. C.
April 6, 1955
Primary view of Incompressible Flutter Characteristics of Representative Aircraft Wings
Wilts, C. H.
June 6, 1955
Primary view of An Investigation of Scaling of Zirconium at Elevated Temperatures Quarterly Status Report no. 9.June 2, 1955 to Sept. 2, 1955
Green, H. M.; Tuchschmid, Heinrich Eugen, 1922- & Baldwin, W. M., Jr.
September 6, 1955
Primary view of An Investigation of the Adaptation of a Transonic Slotted Tunnel to Supersonic Operation by Enclosing the Slots With Fairings
Matthews, Clarence W.
October 6, 1955
Primary view of Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45 Degree Sweptback-Wing Airplane Model With Various Vertical Locations of the Wing and Horizontal Tail: Effect of Wing Location and Geometric Dihedral for the Wing-Body Combination, M = 2.01
Spearman, M. Leroy
April 6, 1955
Primary view of The Mechanical Properties of Beta-Quenched Uranium at Elevated Temperatures
Shober, Frederic R.; Marsh, Lyle L. & Manning, G. K.
September 6, 1955
Primary view of Metallurgical Examination of Resistance Thermometer Elements Removed from 105 KW and KE Areas
Hartcorn, L. A.
June 6, 1955
Primary view of A Numerical Integration Scheme for Problems Involving Contour Representations
Hudson, C. C.
July 6, 1955
Primary view of The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-fuselage-store Configurations 2 - Swept-wing Heavy-bomber Configuration With Large Store Nacelle. Lateral Forces and Pitching Moments, Mach Number, 1.61
Smith, Norman F. & Carlson, Harry W.
July 6, 1955
Primary view of Redox Ventilation Study Recommendation Report
Shaver, B. O. & Nitteberg, L. J.
September 6, 1955
Primary view of Simulator studies of a simple homing system
Passera, Anthony L. & Garner, H. Douglas
October 6, 1955
Primary view of Some Effects of Configuration Variables on Store Loads at Supersonic Speeds
Smith, Norman F. & Carlson, Harry W.
July 6, 1955
Primary view of Stability and drag characteristics of 1/10-scale model of the Convair XF2Y-1 airplane with open inlets containing boundary layer splitter plates as obtained in free flight at Mach numbers between 0.7 and 1.5: TED No. NACA DE 365
Bland, William M., Jr.
April 6, 1955
Primary view of Static Longitudinal and Lateral Stability and Control Characteristics of an 0.065-Scale Model of the Chance Vought Regulus 2 Missile at Mach Numbers of 1.41, 1.61, and 2.01 Research Memorandum
Robinson, Ross B.; Driver, Cornelius & Spearman, M. Leroy
June 6, 1955
Primary view of Static longitudinal and lateral stability and control characteristics of an 0.065-scale model of the Chance Vought Regulus II missile at Mach numbers of 1.41, 1.61, and 2.01: TED No. NACA AD 398
Robinson, Ross B.; Driver, Cornelius & Spearman, M. Leroy
June 6, 1955
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