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A Pressure Distribution Investigation Of The Aerodynamic Characteristics Of A Body Of Revolution In The Vicinity Of A Reflection Plane At Mach Numbers Of 141 And 201
Download A Pressure Distribution Investigation Of The Aerodynamic Characteristics Of A Body Of Revolution In The Vicinity Of A Reflection Plane At Mach Numbers Of 141 And 201 full books in PDF, epub, and Kindle. Read online A Pressure Distribution Investigation Of The Aerodynamic Characteristics Of A Body Of Revolution In The Vicinity Of A Reflection Plane At Mach Numbers Of 141 And 201 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis A Pressure-distribution Investigation of the Aerodynamic Characteristics of a Body of Revolution in the Vicinity of a Reflection Plane at Mach Numbers of 1.41 and 2.01 by : John P. Gapcynski
Download or read book A Pressure-distribution Investigation of the Aerodynamic Characteristics of a Body of Revolution in the Vicinity of a Reflection Plane at Mach Numbers of 1.41 and 2.01 written by John P. Gapcynski and published by . This book was released on 1955 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt: The changes in the aerodynamic characteristics of a body of revolution with a fineness ratio of 8 have been determined at Mach numbers of 1.41 and 2.01, a Reynolds number, based on body length, of 4,540,000, and angles of incidence of 0 degrees and plus or minus 3 degrees as the position of the body is varied with respect to a reflection plane. The data are compared with theoretical results.
Book Synopsis 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 by :
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:
Book Synopsis A Pressure-distribution Investigation of a Fineness-ratio-12.2 Parabolic Body of Revolution (NACA RM-10) at M by : Morton Cooper
Download or read book A Pressure-distribution Investigation of a Fineness-ratio-12.2 Parabolic Body of Revolution (NACA RM-10) at M written by Morton Cooper and published by . This book was released on 1952 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : Louis S. Stiver
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:
Book Synopsis An Experimental Investigation of the Pressure Distribution on Five Bodies of Revolution at Mach Numbers of 2.45 and 3.19 by : G. B. Marson
Download or read book An Experimental Investigation of the Pressure Distribution on Five Bodies of Revolution at Mach Numbers of 2.45 and 3.19 written by G. B. Marson and published by . This book was released on 1954 with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2 by : Edwin J. Saltzman
Download or read book Preliminary Base Pressures Obtained from the X-15 Airplane at Mach Numbers from 1.1 to 3.2 written by Edwin J. Saltzman and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Investigation of Effects of Noise Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 by :
Download or read book A Wind-tunnel Investigation of Effects of Noise Bluntness, Face Shape, and Afterbody Length on the Aerodynamic Characteristics of Bodies of Revolution at Mach Numbers of 2.37, 2.98, and 3.90 written by and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Handbook of Supersonic Aerodynamics by : Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md
Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory, Silver Spring, Md and published by . This book was released on 1961 with total page 516 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of the Drag of Blunt-nosed Bodies of Revolution in Free Flight at Mach Numbers from 0.6 to 2.3 by : Harvey A. Wallskog
Download or read book Investigation of the Drag of Blunt-nosed Bodies of Revolution in Free Flight at Mach Numbers from 0.6 to 2.3 written by Harvey A. Wallskog and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of the Pressure Distribution on Five Bodies of Revolution at Mach Numbers of 2.45 and 3.19 by : College of Aeronautics (Cranfield, Bedfordshire)
Download or read book An Experimental Investigation of the Pressure Distribution on Five Bodies of Revolution at Mach Numbers of 2.45 and 3.19 written by College of Aeronautics (Cranfield, Bedfordshire) and published by . This book was released on 1954 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° by : Leroy Devan
Download or read book Aerodynamics of Tactical Weapons to Mach Number 8 and Angle of Attack 180° written by Leroy Devan and published by . This book was released on 1980 with total page 192 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 by : Ross B. Robinson
Download or read book Effects of Body and Fin Deflections on the Aerodynamic Characteristics in Pitch of a 0.065-scale Model of a Four-stage Rocket Configuration at Mach Numbers of 1.41 and 1.82 written by Ross B. Robinson and published by . This book was released on 1959 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Interference Effects Caused by Parallel-staged Simple Aerodynamic Configurations at Mach Numbers of 3 and 6 by : John P. Decker
Download or read book Aerodynamic Interference Effects Caused by Parallel-staged Simple Aerodynamic Configurations at Mach Numbers of 3 and 6 written by John P. Decker and published by . This book was released on 1969 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics effected by parallel- staged simple aerodynamic configurations at Mach numbers of 3 and 6.
Book Synopsis Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 589 and Mach Numbers to 2 by :
Download or read book Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 589 and Mach Numbers to 2 written by and published by . This book was released on 1979 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0 by : W. F. Lindsey
Download or read book The Flow Past a Straight- and a Swept-wing-body Combination and Their Equivalent Bodies of Revolution at Mach Numbers Near 1.0 written by W. F. Lindsey and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: The complete flow fields past a straight and a swept wing-body combination and their equivalent bodies of revolution at Mach numbers around 1.0 have been observed by means of motion-picture schlieren photography. The results of these observations indicate that the shock growth and positions on the wing-body combinations are closely reproduced in the flow past their respective equivalent bodies.
Book Synopsis An Experimental Investigation of the Base Pressure Characteristics of Nonlifting Bodies of Revolution at Mach Numbers from 2.73 to 4.98 by : John O. Reller
Download or read book An Experimental Investigation of the Base Pressure Characteristics of Nonlifting Bodies of Revolution at Mach Numbers from 2.73 to 4.98 written by John O. Reller and published by . This book was released on 1955 with total page 45 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was undertaken in the Ames 10- by 14-inch supersonic wind tunnel to determine same of the base pressure characteristics of related bodies of revolution at zero angle of attack. The basic body shape used in this investigation was a 10-caliber tangent ogive nose section combined with a cylindrical afterbody. Other related shapes tested differed in that they had either a blunt-nosed profile or a boat-tailed afterbody. Model fineness ratios were varied from 3.12 to 10 by changing afterbody length. Tests were conducted at free-stream Mach changing afterbody length. Tests were conducted at free-stream Mach numbers from 2.73 to 4.98 over a Reynolds number range, based on body length from, 6,000,000 to 8,800,000.
Book Synopsis Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6 by :
Download or read book Effects of Body Shape on the Aerodynamics of a Body of Revolution at Mach Numbers from 1.6 to 4.6 written by and published by . This book was released on 1985 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
