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Primary view of Analysis of Heat and Compressibility Effects in Internal Flow Systems and High-Speed Tests of a Ram-Jet System
Becker, John V. & Baals, Donald D.
July 21, 1942
Primary view of Bibliography of NACA Papers on Rotating-Wing Aircraft, July 1948
Gessow, Alfred
July 21, 1948
Primary view of Effect of a nacelle on the low-speed aerodynamic characteristics of a swept-back wing
Hanson, Frederick H., Jr. & Dannenberg, Robert E.
July 21, 1948
Primary view of Free-Flight Investigation at Transonic and Supersonic Speeds of a Wing-Aileron Configuration Simulating the D-558-2 Airplane
Sandahl, Carl A.
July 21, 1948
Primary view of An investigation at low speed of a 51.3 degrees sweptback semispan wing with a raked tip and with 16.7-percent-chord ailerons having three spans and three trailing-edge angles
Fischel, Jack & Schneiter, Leslie E.
July 21, 1948
Primary view of Measurement Through the Speed of Sound of Static Pressures on the Rear of Unswept and Sweptback Circular Cylinders and on the Rear and Sides of a Wedge by the NACA Wing-Flow Method
Sawyer, Richard H. & Daum, Fred L.
July 21, 1948
Primary view of Study of stress states in gas-turbine disk as determined from measured operating-temperature distributions
Farmer, J. Elmo; Millenson, M. B. & Manson, S. S.
July 21, 1948
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 Monthly Divisional Information Meeting : Isotope Research and Production Division, Y-12
Carbide and Carbon Chemicals Corporation
July 21, 1950
Primary view of Some Effects of Chordwise Fences on the Aerodynamic Characteristics of Four Moderately Sweptback Wings in the Low-Lift Range at Transonic Mach Numbers and at Mach Number 1.9
Guy, Lawrence D.
July 21, 1950
Primary view of Terminal report on the Radiolanthanum Laboratory
Figenshau, J. K.
July 21, 1950
Primary view of Terminal Report on the Radiolanthanum Laboratory
Figenshau, J. K.
July 21, 1950
Primary view of The Effects of Internal Conversion on Critical Mass and Operating Life of a Thermal Reactor
Snyder, T. M.
July 21, 1952
Primary view of Examination of Discharged Process Tubes
Dalrymple, R. S.
July 21, 1952
Primary view of Pressure Distributions on Bodies of Revolution at Subsonic and Transonic Speeds
Cole, Richard I.
July 21, 1952
Primary view of Reflection of shock waves from slotted walls at Mach number 1.62
Wood, George P.
July 21, 1952
Primary view of Water Adsorbed by Graphite at Various Relative Pressures
Spalaris, C. N.
July 21, 1953
Primary view of Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Longitudinal Stability and Control of the Model Equipped with a Supersonic-Type Elliptical Wing-Root Inlet
Kelly, H. Neale & Cancro, Patrick A.
July 21, 1954
Primary view of Table Top 1 Circuitry
Cummings, David B. & Wharton, Charles B.
July 21, 1954
Primary view of Buckling of an Elliptic Cylinder First Roots of the Zero Order, Modified Mathieu Function
Gast, Paul F. & Bournis, Anthony
July 21, 1955
Primary view of An experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations
Carlson, Harry W. & Gapcynski, John P.
July 21, 1955
Primary view of Flight Measurements of Horizontal-Tail Loads on the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Degrees
Reed, Robert D.
July 21, 1955
Primary view of Load distributions on wings and wing-body combinations at high angles of attack and supersonic speeds
Katzen, Elliott D. & Pitts, William C.
July 21, 1955
Primary view of Stability and control characteristics obtained during demonstration of the Douglas X-3 research airplane
Day, Richard E. & Fischel, Jack
July 21, 1955
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