National Advisory Committee for Aeronautics (NACA) - 116 Matching Results

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Primary view of The Knock-Limited Performance of Fuel Blends Containing Spiropentane, Methylenecyclobutane, Di-Tert-Butyl Ether, Methyl Tert-Butyl Ether, and Triptane
Meyer, Carl L.
May 1946
Primary view of Effects of Fuel-Vapor Loss on Knock-Limited Performance and Inspection Properties of Aviation Fuels
Barnett, Henry C. & Marsh, Edred T.
March 1946
Primary view of Aerodynamic Characteristics of Four NACA Airfoil Sections Designed for Helicopter Rotor Blades
Stivers, Louis S., Jr. & Rice, Fred J., Jr.
February 1946
Primary view of An analysis of the fatigue life of an airplane wing structure under overload conditions
Putnam, Abbott A. & Reisert, Thomas D.
February 1946
Primary view of Lead Susceptibility of Several Fuels as Determined in an Air-Cooled Aircraft-Engine Cylinder
Stricker, Edward G. & Hensley, Reece V.
February 1946
Primary view of Static-Pressure Error of an Airspeed Installation on an Airplane in High-Speed Dives and Pullouts
Zalovcik, John A. & Wood, Clotaire
February 1946
Primary view of Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 6 Degrees and 9 Degrees Trim and a 22-1/2 Degree Angle of Dead Rise
Batterson, Sidney A. & Stewart, Thelma
February 1946
Primary view of Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 12 Degree Trim and With a 22-1/2 Degree Angle of Dead Rise
Batterson, Sidney A.
February 1946
Primary view of A Method for the Determination of Aromatics in Hydrocarbon Mixtures
Hipsher, Harold F.
December 1945
Primary view of The Knock-Limited Performance of S Reference Fuel Plus 2 Milliliters of Triethylthallium Per Gallon
Meyer, Carl L.
November 1945
Primary view of Use of Variable-Ratio Geared Tabs to Improve Stick-Force Characteristics in Turning Flight
Kleckner, Harold F.
October 1945
Primary view of An Approximate Determination of the Power Required to Move Control Surfaces as Related to Control-Booster Design
Johnson, Harold I.
September 1945
Primary view of Comparative Fatigue Tests of Riveted Joints of Alclad 24S-T, Alclad 24S-T81, Alclad 24S-RT, Alclad 24S-T86 and Alclad 75S-T Sheet
Moore, R. L. & Hill, H. N.
August 1945
Primary view of A Comparison of Data Obtained by Two Flight Techniques for Determining the Sideslip Characteristics of a Fighter Airplane
Johnson, Harold I.
August 1945
Primary view of Computation of the Mean Tangential Velocity of the Air Leaving the Blade Tips of a Centrifugal Supercharger
Brown, W. Byron
August 1945
Primary view of Effect of Variation in Diameter and Pitch of Rivets on Compressive Strength of Panels With Z-Section Stiffeners 1 - Panels With Close Stiffener Spacing That Fail by Local Buckling
Dow, Norris F. & Hickman, William A.
August 1945
Primary view of Comparison of Structural Efficiencies of Diagonal-Tension Webs and Truss Webs of 24S-T Aluminum Alloy
Ochiltree, David W.
July 1945
Primary view of Pressure Lag in Tubing Used in Flight Research
Turner, Howard L. & Rathert, George A., Jr.
July 1945
Primary view of Tables and Charts for the Evaluation of Profile Drag From Wake Surveys at High Subsonic Speeds
Block, Myron J. & Katzoff, S.
July 1945
Primary view of Theoretical and Experimental Dynamic Loads for a Prismatic Float Having an Angle of Dead Rise of 22-1/2 Degrees
Mayo, Wilbur L.
July 1945
Primary view of Determination From Flight Tests of Thrust Coefficients for 10 Full-Scale Airplanes in the Gliding Condition With Engine Idling
Talmage, Donald B.
June 1945
Primary view of Fuel-Evaporation Loss as Determined by the Change in the Specific Gravity of the Fuel in an Aircraft Fuel Tank
Stone, Charles S. & Kramer, Walter E.
May 1945
Primary view of Investigation of Methods of Supporting Single-Thickness Specimens in a Fixture for Determination of Compressive Stress-Strain Curves
Kotanchik, Joseph N.; Woods, Walter & Weinberger, Robert A.
May 1945
Primary view of Effects of Compressibility and Large Angles of Yaw on Pressure Indicated by a Total-Pressure Tube
Humphreys, Milton D.
April 1945
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