Download or read book Wind tunnel Pressure Measurements in the Wake of a Cone cylinder Model at Mach Numbers of 2 30 and 4 65 written by John T. McShera and published by . This book was released on 1965 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1974 with total page 992 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Contractor Report written by and published by . This book was released on 1970 with total page 746 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Experimental Study of the Turbulent Wake Behind a Cone at Mach 5 written by William C. Ragsdale and published by . This book was released on 1966 with total page 166 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental study of the turbulent wake behind a 9° adiabatic cone at Mach 5 has been carried out in the U.S. Naval Ordnance Laboratory Hypersonic Tunnel. Cone models with base diameters of 2 inches and 4 inches were mounted in the wind tunnel test section with fine wires. Pitot pressure, pressure on a small cone probe and total temperature were measured with probes mounted on a vertical traversing mechanism. The measured pressures and temperatures were used to calculate the Mach number, static pressure, static temperature, velocity and density in the wake.
Download or read book Wind tunnel Measurements at Mach Numbers from 3 to 5 of Pressure and Turbulent Heat Transfer on a Blunt Cone cylinder with Flared Afterbody written by Mamoru Inouye and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on with total page 812 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Volume of Technical Papers written by and published by . This book was released on 1966 with total page 258 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 United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1966 with total page 2088 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Experimental Study of the Turbulent Wake Behind a Cone at Mach 5 written by and published by . This book was released on 1966 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental study of the turbulent wake behind a 9 degree adiabatic cone at Mach 5 was carried out. Cone models with base diameters of 2 inches and 4 inches were mounted in the wind tunnel test section with fine wires. Pitot pressure, pressure on a small cone probe and total temperature were measured with probes mounted on a vertical traversing mechanism. The measured pressures and temperatures were used to calculate the Mach number, static pressure, static temperature, velocity and density in the wake. (Author).
Download or read book Wind tunnel Pressure Data at Mach Numbers from 1 6 to 4 63 for a Series of Bodies of Revolution at Angles of Attack from 4 to 60 written by Emma Jean Landrum and published by . This book was released on 1977 with total page 156 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Measurements of Pressure and Local Heat Transfer on a 20 Cone at Angles of Attack Up to 20 for a Mach Number of 4 95 written by Jerome D. Julius and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of Reynolds Number Effects for a Series of Cone cylinder Bodies at Mach Number of 1 62 1 93 and 2 41 written by Carl E. Grigsby and published by . This book was released on 1953 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: An investigation of the Reynolds number for transition and the skin-friction drag at zero lift of eight cone-cylinder bodies having varying fineness ratios has been made at Mach numbers of 1.62, 1.93, and 2.41 over a Reynolds number range from 0.3 x 106 to 10 x 106. The accuracy of the skin-friction data was not sufficient to permit any general conclusions to be drawn. The Reynolds number for transition was found to be dependent upon both the tunnel stagnation pressure and Mach number.
Download or read book NASA SP written by and published by . This book was released on 1993 with total page 590 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Measurements on a Blunt Cone at Mach Numbers from 1 7 to 7 6 for Allied Research Associates Inc written by William C. Noz and published by . This book was released on 1961 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at Mach Numbers from 1 47 to 4 62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact written by and published by . This book was released on 1961 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Heat transfer and Pressure Measurements on a Concave nose Cylinder for Mach Number Range of 2 49 to 4 44 written by and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Index Aeronauticus written by and published by . This book was released on 1966 with total page 976 pages. Available in PDF, EPUB and Kindle. Book excerpt:
