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Experimental Investigation Of The Drag Of 30 Degrees 60 Degrees And 90 Degrees Cone Cylinders At Mach Numbers Between 15 And 82
Download Experimental Investigation Of The Drag Of 30 Degrees 60 Degrees And 90 Degrees Cone Cylinders At Mach Numbers Between 15 And 82 full books in PDF, epub, and Kindle. Read online Experimental Investigation Of The Drag Of 30 Degrees 60 Degrees And 90 Degrees Cone Cylinders At Mach Numbers Between 15 And 82 ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Experimental Investigation of the Drag of 30 Degrees, 60 Degrees, and 90 Degrees Cone Cylinders at Mach Numbers Between 1.5 and 8.2 by : Alvin Seiff
Download or read book Experimental Investigation of the Drag of 30 Degrees, 60 Degrees, and 90 Degrees Cone Cylinders at Mach Numbers Between 1.5 and 8.2 written by Alvin Seiff and published by . This book was released on 1952 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Drag of 30-, 60-, and 90-degree Cone Cylinders at Mach Numbers Between 1.5 and 8.2 by : Alvin Seiff
Download or read book Experimental Investigation of the Drag of 30-, 60-, and 90-degree Cone Cylinders at Mach Numbers Between 1.5 and 8.2 written by Alvin Seiff and published by . This book was released on 1952 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Drag of 30°, 60°, and 90° Cone Cylinders at Mach Numbers Between 1.5 and 8.2 by : Alvin Seiff
Download or read book Experimental Investigation of the Drag of 30°, 60°, and 90° Cone Cylinders at Mach Numbers Between 1.5 and 8.2 written by Alvin Seiff and published by . This book was released on 1952 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Stability and Drag of a Pointed and a Blunted 30 Degrees Half-angle Cone at Mach Numbers from 11.5 to 34 in Air by : Peter F. Intrieri
Download or read book Experimental Stability and Drag of a Pointed and a Blunted 30 Degrees Half-angle Cone at Mach Numbers from 11.5 to 34 in Air written by Peter F. Intrieri and published by . This book was released on 1966 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Reynolds Number Effects for a Series of Cone-cylinder Bodies at Mach Number of 1.62, 1.93, and 2.41 by : Carl E. Grigsby
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.
Book Synopsis U.S. Government Research & Development Reports by :
Download or read book U.S. Government Research & Development Reports written by and published by . This book was released on 1970 with total page 1298 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of the Effect of Surface Roughness of the Drag of a Cone-cylinder Model at a Mach Number of 2.48 by : John Henry Terry Wade
Download or read book An Experimental Investigation of the Effect of Surface Roughness of the Drag of a Cone-cylinder Model at a Mach Number of 2.48 written by John Henry Terry Wade and published by . This book was released on 1955 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U. S. Government Research and Development Reports by :
Download or read book U. S. Government Research and Development Reports written by and published by . This book was released on 1970 with total page 1296 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Wind-tunnel Investigation of Forces on Cones at Low Mach Numbers by : David Litwack
Download or read book A Wind-tunnel Investigation of Forces on Cones at Low Mach Numbers written by David Litwack and published by . This book was released on 1965 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The investigation was conducted to obtain subsonic aerodynamic forces on cones. Nine aluminum cones varying in apex angel from 10 degrees to 90 degrees were tested. Lift, drag and pitching moment were measured at angles of attack varying from -5 deg. to 180 deg. in 10 degree increments and at a dynamic pressure of up to 200 lb./sq. ft. The measured data was first corrected for tare and interference effects; three-dimensional wind-tunnel-boundary-corrections were then applied to correct the data to free-air conditions. This data is presented in graphical form as lift, drag and pitching moment coefficient versus angle of attack for each cone. A plot of drag coefficient versus Reynolds Number at each angle of attack for the 30 degree cone and the 60 degree cone showed the drag almost constant for each angle of attack over the small range of Reynolds Numbers tested (Re = 15,000 to Re = 57,000). The maximum lift to drag ratio for the three smallest cones (10 deg. to 30 deg. cone apex angle) occurred at an angle of attack between 30 deg. to 40 deg.; for every other cone (40 deg. to 90 deg. cone apex angle) the maximum L/D was at an angle of attack between 120 deg. and 130 deg. (Author).
Book Synopsis Government Reports Announcements by :
Download or read book Government Reports Announcements written by and published by . This book was released on 1970 with total page 1084 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of the Turbulent-boundary-layer Temperature-recovery Factor on Bodies of Revolution at Mach Numbers from 2.0 to 3.8 by : Howard A. Stine
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.
Book Synopsis International Aerospace Abstracts by :
Download or read book International Aerospace Abstracts written by and published by . This book was released on 1999 with total page 974 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 by : Peter F. Intrieri
Download or read book Free-flight Measurements of the Static and Dynamic Stability and Drag of a 10 Degree Blunted Cone at Mach Numbers 3.5 and 8.5 written by Peter F. Intrieri and published by . This book was released on 1962 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Towed Cones Used as Decelerators at Mach Numbers from 1.57 to 4.65 by : Nickolai Charczenko
Download or read book Aerodynamic Characteristics of Towed Cones Used as Decelerators at Mach Numbers from 1.57 to 4.65 written by Nickolai Charczenko and published by . This book was released on 1962 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: Towed and sting-supported cones were tested in the wake of various payloads at supersonic speeds to determine their drag and stability characteristics. The investigation extended over a Mach number range from 1.57 to 4.65 and included such variables as Reynolds number, cone angle, ratio of cone base diameter to payload base diameter, and trailing distance. Cones towed in the wake of a symmetrical payload at supersonic speeds, in general, had good drag and stability characteristics if towed in the supersonic flow region. A cone with an included angle between 80 and 90 degrees gave 2 maximum drag while still maintaining stability. In order to minimize wake effects, the ratio of cone base diameter to payload base diameter should be at least one and preferably around three. A trailing distance of three times the payload base diameter, in most cases, is of sufficient length to avoid low drag and instability of the decelerator. (Author).
Book Synopsis Government Reports Announcements & Index by :
Download or read book Government Reports Announcements & Index written by and published by . This book was released on 1970 with total page 1310 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Stability and Drag of a Pointed and a Blunted 30 ̊half-angle Cone at Mach Numbers from 11.5 to 34 in Air by : Peter F. Intrieri
Download or read book Experimental Stability and Drag of a Pointed and a Blunted 30 ̊half-angle Cone at Mach Numbers from 11.5 to 34 in Air written by Peter F. Intrieri and published by . This book was released on 1966 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Bibliography of Scientific and Industrial Reports by :
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1969 with total page 834 pages. Available in PDF, EPUB and Kindle. Book excerpt:
