Technical Report Archive & Image Library (TRAIL) - 27 Matching Results

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Primary view of Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2: Pressure and force measurements at Mach numbers of 1.52 and 1.98
Perkins, Edward W.; Gowen, Forrest E. & Jorgensen, Leland H.
September 19, 1951
Primary view of Analysis of measured pressures on airfoils at Mach numbers near 1
Habel, Louis W. & Miller, Mason F.
September 19, 1949
Primary view of Conference on "Hot" Laboratory Design Held at Brookhaven National Laboratory on September 19, 1947
Strickland, Gerald
September 19, 1951
Primary view of Corrosivity of Uranyl Fluoride to Certain Metals
Little, L. F. & Susano, C. D.
September 19, 1946
Primary view of A Countercurrent Solid-Liquid Contactor for Continuous Ion Exchange
Higgins, I. R.
September 19, 1952
Primary view of Cyclic engine operation of cast vitallium turbine blades at an exhaust-cone gas temperature of 1440 plus or minus 20 F
Yaker, Charles & Garrett, Floyd B.
September 19, 1949
Primary view of Design and test of mixed-flow impellers 1: aerodynamic design procedure
Osborn, Walter M. & Hamrick, Joseph T.
September 19, 1952
Primary view of Design and Test of Mixed-Flow Impellers 2: Experimental Results, Impeller Model MFI-1A
Withee, Joseph R., Jr. & Beede, William L.
September 19, 1952
Primary view of Effect of Full-Span Trailing-Edge Elevons on the Transonic Longitudinal Aerodynamic Characteristics of a Wing-Body Combination Having a 3-Percent-Thick Triangular Wing With 60 Degree Leading-Edge Sweep
Critzos, Chris C. & Foss, Willard E., Jr.
September 19, 1957
Primary view of Effect of the Proximity of the Ground on the Stability and Control Characteristics of a Vertically Rising Airplane Model in the Hovering Condition
Smith, Charles C., Jr.; Lovell, Powell M., Jr. & Bates, William R.
September 19, 1951
Primary view of Effects on the weight-flow range and efficiency of a typical axial-flow compressor inlet stage that result from the use of a decreased blade camber or decreased guide-vane turning
Jackson, Robert J.
September 19, 1952
Primary view of Experimental heat-transfer and friction coefficients for air flowing through stacks of parallel flat plates
Sams, Eldon W. & Weiland, Walter F., Jr.
September 19, 1954
Primary view of Factors Affecting the Design of Quiet Propellers
Regier, Arthur A. & Hubbard, Harvey H.
September 19, 1947
Primary view of Free-flight investigation of jet effect on the low-lift drag and longitudinal trim of a supersonic interceptor-type airplane configuration with an overhanging tail boom at Mach numbers from 1.09 to 1.34
Blanchard, Willard S., Jr.
September 19, 1957
Primary view of Gamma-Induced Light Production in Water
Rich, J. A. & Slovacek, R. E.
September 19, 1952
Primary view of Homogeneous Reactor Project Quarterly Progress Report: July 1952
Swartout, J. A.; Secoy, C. H.; Winters, C. E. & Thompson, William E., 1923-
September 19, 1952
Primary view of An introduction to the physical aspects of helicopter stability
Gessow, Alfred & Amer, Kenneth B.
September 19, 1949
Primary view of Investigation at Mach Number 1.88 of Half of a Conical-Spike Diffuser Mounted as a Side Inlet With Boundary-Layer Control
Goelzer, H. Fred & Cortright, Edgar M., Jr.
September 19, 1951
Primary view of Longitudinal frequency-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements, including a method for the evaluation of transfer functions
Triplett, William C. & Smith, G. Allan
September 19, 1951
Primary view of Report on Investigation of Developed Turbulence
Prandtl, L.
September 19, 1949
Primary view of The Rolling Friction of Several Airplane Wheels and Tires and the Effect of Rolling Friction on Take-Off
Wetmore, J. W.
September 19, 1936
Primary view of Schlieren investigation of the wing shock-wave boundary-layer interaction in flight
Cooper, George E. & Bray, Richard S.
September 19, 1951
Primary view of Some approximate equations for the standard atmosphere
Diehl, Walter S.
September 19, 1930
Primary view of Some Effects of Nonlinear Variation in the Directional-Stability and Damping-in-Yawing Derivatives on the Lateral Stability of an Airplane
Sternfield, Leonard
September 19, 1950
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