Download or read book Investigation of the Laminar Aerodynamic Heat transfer Characteristics of a Hemisphere cylinder in the Langley 11 inch Hypersonic Tunnel at a Mach Number of 6 8 written by Davis H. Crawford and published by . This book was released on 1956 with total page 680 pages. Available in PDF, EPUB and Kindle. Book excerpt: At the stagnation point, the theory of Sibulkin, using the diameter and conditions behind the normal shock, was in good agreement with the experiment when the velocity graident at the stagnation opint appropriate to the free-stream Mach number was used.
Download or read book Investigation of the Compressive Strength and Creep of 7075 T6 Aluminum alloy Plates at Elevated Temperatures written by William D. Deveikis and published by . This book was released on 1957 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt: Elevated-temperature compressive-strength test results from room temperature to 600 degrees F and creep test results from 350 degrees F to 500 degrees F are presented for V-groove edge-supported plates of 7075-T6 aluminum alloy. The test data are compared with calculations obtained from procedures for estimating maximum strength from material stress-strain curves and creep-failure stresses from isochronous stress-strain curves. The strength and creep results from this investigation are also compared with similar results from 2024-T3 aluminum-alloy plates.
Download or read book WADC Technical Report written by United States. Wright Air Development Division and published by . This book was released on 1959 with total page 1318 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book U S Government Research Reports written by and published by . This book was released on 1957 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental and Predicted Longitudinal and Lateral directional Response Characteristics of a Large Flexible 35 Swept wing Airplane at an Altitude of 35 000 Feet written by Clarence A. Syvertson and published by . This book was released on 1957 with total page 304 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 1958 with total page 1136 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Some Mechanical Properties of Thermenol Compressor Blades written by Donald F. Johnson and published by . This book was released on 1957 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt: Comparison in bending and torsional deflection tests showed thermenol to have a modulus of elasticity of about 26,000,000 and a modulus of rigidity of abot 9,000,000.
Download or read book NACA Conference on Aircraft Loads Structures and Flutter written by and published by . This book was released on 1957 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Heat transfer and Pressure Distributions at Mach Numbers of 6 0 and 9 6 Over Two Reentry Configurations for the Five stage Scout Vehicle written by Paul F. Holloway and published by . This book was released on 1963 with total page 64 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 1956 with total page 342 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NACA Conference on High Speed Aerodynamics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1958 with total page 678 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Local Heat Transfer to Blunt Noses at High Supersonic Speeds written by William E. Stoney and published by . This book was released on 1957 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Pressure Distributions Over Blunt Two and Three dimensional Bodies Having Similar Cross Sections at a Mach Number of 4 95 written by Jerome D. Julius and published by . This book was released on 1959 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1971 with total page 902 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Local Aerodynamic Heat Transfer and Boundary layer Transition on Roughened Sphere ellipsoid Bodies at Mach Number 3 0 written by William D. Deveikis and published by . This book was released on 1961 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Report written by and published by . This book was released on 1962 with total page 722 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of an Oblate Spheroid and a Sphere at Mach Numbers from 1 70 to 10 49 written by Lloyd S. Jernell and published by . This book was released on 1970 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Drag coefficients of oblate spheroid and sphere at Mach numbers from 1.70 to 10.49.
