National Advisory Committee for Aeronautics (NACA) - 193 Matching Results

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Primary view of Performance of B. M. W. 185-horsepower airplane engine
Sparrow, Stanwood Willston
April 13, 1922
Primary view of Experimental Evaluation of Swirl Can Elements for Hydrogen Fuel Combustor
Rayle, Warren D.; Jones, Robert E. & Friedman, Robert
May 13, 1957
Primary view of Ditching investigation of a 1/25-scale model of a 255,000-pound transport airplane
Windham, John O.
July 13, 1955
Primary view of The effect of blunt-trailing-edge elevons on the longitudinal and lateral handling qualities of the semitailless airplane
Saltzman, Edwin J.
January 13, 1955
Primary view of Stabilization of 50-Percent Magnesium - JP-4 Slurries With Some Aluminum Soaps of C(Sub 8) Acids
Caves, Robert M.
May 13, 1954
Primary view of Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy
Smiley, Robert F.
January 13, 1956
Primary view of Free-Spinning-Tunnel Investigation of a 1/28-Scale Model of the North American FJ-4 Airplane
Healy, Frederick M.
January 13, 1958
Primary view of Effect of NACA Injection Impeller and Ducted Head Baffles on Flight Cooling Performance of Double-Row Radial Engine in Four-Engine Heavy Bomber
Marble, Frank E.; Miller, Mahlon A. & Vensel, Joseph R.
April 13, 1945
Primary view of Effectiveness of Thermal-Pneumatic Airfoil-Ice-Protection System
Gowan, William H., Jr. & Mulholland, Donald R.
April 13, 1951
Primary view of Effects of Free-Stream Reynolds Number, Engine Installation, and Model Scale on Stability Characteristics of a Translating-Spike Inlet at Mach 2.0
Musial, Norman T. & Bowditch, David
November 13, 1957
Primary view of Effect of Design Changes of Operating Conditions on Combustion and Operational Performance of a 28-Inch Diameter Ram-Jet Engine
Shillito, T. B. & Nakanishi, Shigeo
February 13, 1952
Primary view of Experimental investigation of velocity distributions of downstream of single duct bends
Weske, John R.
January 13, 1947
Primary view of A Wind-Tunnel Investigation of the Stability of the Antisubmarine Rocket Mk 1 Mod 0
Lichtenstein, Jacob H. & Williams, James L.
November 13, 1952
Primary view of Experimental Investigation of Extreme Internal Flow Turning at the Cowl Lip of an Axisymetric Inlet at a Mach Number of 2.95
Weston, Kenneth C. & Kowalski, Kenneth L.
May 13, 1958
Primary view of The Origin and Distribution of Supsonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 5 - Swept-Wing Heavy-Bomber Configuration With Large Store (Nacelle). Mach Number, 2.01
Carlson, Harry W. & Geier, Douglas J.
February 13, 1956
Primary view of Free-Flight Aerodynamic-Heating Data at Mach Numbers Up to 10.9 on a Flat-Faced Cylinder
Bland, William M., Jr.; Swanson, Andrew G. & Kolenkiewicz, Ronald
January 13, 1958
Primary view of Theoretical Investigation of the Performance of Proportional Navigation Guidance Systems-Effect of Method of Positioning the Radar Antenna on the Speed of Response
Abramovitz, Marvin
August 13, 1952
Primary view of Thermal Stability of a Commercial Propyl Pentaborane (HEF-2) in the Range 147 Degree to 190 Degree C
McDonald, G.
November 13, 1957
Primary view of Investigation of an Underslung Scoop Inlet at Mach Numbers to 1.99
Weinstein, Maynard I.; Vargo, Donald J. & McKevitt, Frank
March 13, 1957
Primary view of Drag at Model Trim Lift of a 1/15-Scale Convair B-58 Supersonic Bomber
Hopko, Russell N. & Kinard, William H.
July 13, 1956
Primary view of Investigation of shock diffusers at Mach number 1.85 3: multiple-shock and curved-contour projecting cones
Moeckel, W. E. & Connors, J. F.
August 13, 1947
Primary view of An investigation of the effect of tip shape on the low-speed aerodynamic characteristics of large-scale swept wings
Walling, Walter C.
November 13, 1947
Primary view of Free-Flight Investigation of Fullspan, 0.2 Chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Taper, Aspect Ratio, and Section-Thickness Ratio
Sandahl, Carl A.
August 13, 1947
Primary view of Theoretical analysis of the performance of a supersonic ducted rocket
Hensley, Reece V.
February 13, 1948
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