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 Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Aerodynamic Characteristics of Two Blunted Cone Reentry Configurations at Mach Numbers from 17 6 to 22 2 Including Some Reynolds Number Effects written by Dal V. Maddalon and published by . This book was released on 1966 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Variation with Reynolds Number of the Base Wave and Skin friction Drag of a Parabolic Body of Revolution NACA RM 10 at Mach Numbers of 1 62 1 93 and 2 41 in the Langley 9 inch Supersonic Tunnel written by Eugene S. Love and published by . This book was released on 1952 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Reynolds Number and Flow Incidence on the Force Characteristics of a Family of Flat front Cylinders written by Vernard E. Lockwood and published by . This book was released on 1967 with total page 50 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 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 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 Flow Incidence and Reynolds Number on Low speed Aerodynamic Characteristics of Several Noncircular Cylinders with Applications to Directional Stability and Spinning written by Edward Charles Polhamus 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 Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone cylinder Configurations at a Mach Number of 6 83 and Angles of Attack Up to 1300 written by Jim A. Penland and published by . This book was released on 1961 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0 30 to 2 85 written by Lucille C. Coltrane and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Investigation of Sharp Cone cylinder Spikes on 120 blunted Cones at Mach Numbers of 3 00 4 50 and 6 00 written by Robert J. McGhee and published by . This book was released on 1969 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Study of the Effects of Reynolds Number and Mach Number on Constant Pressure Coefficient Jump for Shock induced Trailing edge Separation written by Atlee M. Cunningham and published by . This book was released on 1987 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Wind tunnel Investigation of the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2 37 2 98 and 3 90 at Angles of Attack to 90 Deg written by and published by . This book was released on 1960 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Investigation of Reynolds Number Effects on a Tangent ogive Cylinder Body written by L. C. Ward and published by . This book was released on 1992 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Investigation of the Turbulent boundary layer Temperature recovery Factor on Bodies of Revolution at Mach Numbers from 2 0 to 3 8 written by Howard A. Stine and published by . This book was released on 1952 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: A turbulent-boundary-layer temperature recovery factor f 0.885 plus or minus 0.011 was measured on both a 10 degree cone and a 40 degree cone cylinder at Mach numbers from 2 to 3.8 and Reynolds numbers based on surface kinematic viscosity from 400,000 to 4,000,000. Comparisons are made with available theories and experiments.
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:
