Download or read book Effects of Propeller Operation and Angle of Yaw on the Distribution of the Load on the Horizontal Tail Surface of a Typical Pursuit Airplane written by Harold H. Sweberg and published by . This book was released on 1944 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements were made in the NACA full-scale tunnel of the pressure distribution over the horizontal tail surface of a typical pursuit airplane in order to determine the effects of propeller operation and angle of yaw on the tail load distribution. Most of the tests were made with the propeller operating to simulate climb conditions, high-speed dives, and pull-ups to various normal accelerations for angles of yaw ranging from 10 degrees to -10 degrees. Measurements were also made of the distributions of downwash angle and dynamic pressure in front of the horizontal tail and results have been correlated with the results of the pressure-distribution tests.
Download or read book NACA Wartime Reports Series L written by Harold H. Sweberg and published by . This book was released on 1944 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt: The pressure distribution had been measured at several longitudinal sections of the vertical tail surface of the Curtiss P-40K airplane in the NACA full-scale tunnel. The tests were made for various angles of attack and angles of yaw with the propeller removed and with the propeller operating. These tests were incidental to a similar investigation of the horizontal-tail loading.
Download or read book Measurements of the Pressure Distribution on the Horizontal Tail Surface of a Typical Propeller driven Pursuit Airplane in Flight written by Melvin Sadoff and published by . This book was released on 1947 with total page 17 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements were made in sideslipping flight at a Mach number of 0.50 of the pressure distribution over the horizontal tail surfaces of a tractor-propeller-driven pursuit airplane, to determine the effects of angle of sideslip and propeller operation on the tail-load distribution. Measurements were also made on the tail-load distribution on the horizontal tail in steady unaccelerated flight over a Mach number range of 0.30 to 0.79 and 0.30 to 0.74, respectively, for the power-on and power-off conditions.
Download or read book Flight Measurements of Aerodynamic Loads on the Horizontal Tail Surface of a Fighter type Airplane written by John B. Garvin and published by . This book was released on 1947 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt: A series of flight measurements of the loads applied to the horizontal tail surfaces of a fighter-type airplane were made. The results were analyzed and found to verify the fact that a knowledge of the tail-load parameters will permit the calculation of the horizontal-tail load. The influence of sideslip on the horizontal-tail load was determined and the critical conditions for design are enumerated.
Download or read book Wartime Report written by and published by . This book was released on 194? with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt: Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Download or read book NACA Wartime Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 586 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1949 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Note written by and published by . This book was released on 1947 with total page 434 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wartime Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on with total page 258 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1947 with total page 914 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Charts of Thermodynamic Properties of Air and Combustion Products from 300 to 3500 R written by Robert E. English and published by . This book was released on 1950 with total page 706 pages. Available in PDF, EPUB and Kindle. Book excerpt: Numerical examples illustrate application of charts to thermodynamic computations for gas-turbine engines.
Download or read book A Study of NACA and NASA Published Information of Pertinence in the Design of Light Aircraft written by James C. Williams and published by . This book was released on 1970 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report investigates critical reviews of NACA and NASA report literature on aerodynamics and aerodynamic load calculations for light aircraft design.
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1949 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Charts of Pressure Rise Obtainable with Airfoil type Axial flow Cooling Fans written by A. Kahane and published by . This book was released on 1947 with total page 578 pages. Available in PDF, EPUB and Kindle. Book excerpt: Charts are presented to show the pressure rise that is obtainable in an engine-cooling installation with a typical airfoil-type propeller-speed fan. The charts cover fans of the stator-rotor, rotor-stator, and rotor alone configurations, with blades incorporating both the highly cambered 65-series blower-blade sections and the conventional low-cambered airfoil sections. The effects of operation of a geared fan with rotational speeds limited by compressibility considerations and the effects of initial rotational inflow are indicated. Use of the charts to predict the pressure rise obtainable with any fan of the types considered is illustrated in a sample calculation.
Download or read book Diagonal Tension in Curved Webs written by Paul Kuhn and published by . This book was released on 1947 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt: The engineering theory of incomplete diagonal tension in plane webs presented in NACA TN No. 1364 is generalizd in order to make it applicable to curved webs. Comparisons are given between calculated and experimental results for a number of stiffened cylinders subjected to torsional loads. The results indicate that the theory predicts the stresses to about the same accuracy for curved webs as for plane webs. The failing stresses in the stringers in curved webs were predicted conservatively in all cases.
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1947 with total page 1314 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Effect of Angle of Sideslip and Propeller Operation written by Melvin Sadoff and published by . This book was released on 1947 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:
