Download or read book Comparison of Experimental and Theoretical Normal force Distributions including Reynolds Number Effects on an Ogive cylinder Body at Mach Number 1 98 written by Edward W. Perkins and published by . This book was released on 1954 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: Normal-force and pressure distributions have been determined for a body of revolution consisting of a fineness-ratio-3, circular-arc, ogival nose tangent to a cylindrical afterbody 7 diameters long. The free-stream Mach number was 1.98; the angle-of-attack range was from 0 to 20 degrees; and the Reynolds numbers, based on body diameter, were 150,000 and 450,000.
Download or read book U S Government Research Reports written by and published by . This book was released on 1956 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1954 with total page 800 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Israel Journal of Technology written by and published by . This book was released on 1966 with total page 298 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes proceedings of various meetings and conferences.
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1956 with total page 1174 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 1966 with total page 1492 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1998 with total page 984 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 Effect of Reynolds Number on the Force and Pressure Distribution Characteristics of a Two Dimensional Lifting Circular Cylinder written by Vernard E. Lockwood and published by . This book was released on 1960 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Measured and Theoretical Flow Fields Behind a Rectangular and a Triangular Wing Up to High Angles of Attack at a Mach Number of 2 46 written by Frank J. Centolanzi and published by . This book was released on 1959 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1952 with total page 136 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 Effects of Reynolds Number on the Stability of a Blunt nosed Flared Cylinder from Mach 17 6 to 22 2 in Helium written by and published by . This book was released on 1965 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Unit Reynolds Number Nose Bluntness Angle of Attack and Roughness on Transition on a 5 Half angle Cone at Mach 8 written by P. Calvin Stainback and published by . This book was released on 1969 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Summary of Static Stability and Drag Characteristics of Axisymmetric Low drag Shapes for the Subsonic to Hypersonic Mach Number Range written by Amado A. Trujillo and published by . This book was released on 1968 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Calculated Pressure Distributions and Components of Total drag Coefficients for 18 Constant volume Slender Bodies of Revolution at Zero Incidence for Mach Numbers from 2 0 to 12 0 with Experimental Aerodynamic Characteristics for Three of the Bodies written by Louis S. Stiver and published by . This book was released on 1971 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Jet Billowing on Stability of Missile type Bodies at Mach 3 85 written by Reino J. Salmi and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
