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Effect Of Jet Pluming On The Static Stability Of Cone Cylinder Flare Configurations As A Mach Number Of 965
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Book Synopsis Effect of Jet Pluming on the Static Stability of Cone-cylinder-flare Configurations as a Mach Number of 9.65 by : William F. Hinson
Download or read book Effect of Jet Pluming on the Static Stability of Cone-cylinder-flare Configurations as a Mach Number of 9.65 written by William F. Hinson and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Jet Pluming on the Static Stability of Cone-cylinder-flare Configurations as a Mach Number of 9.65 by : William F. Hinson
Download or read book Effect of Jet Pluming on the Static Stability of Cone-cylinder-flare Configurations as a Mach Number of 9.65 written by William F. Hinson and published by . This book was released on 1962 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Jet Pluming on the Static Stability of Cone-cylinder-flare Configurations as a Mach Number of 9.65 by : William F. Hinson
Download or read book Effect of Jet Pluming on the Static Stability of Cone-cylinder-flare Configurations as a Mach Number of 9.65 written by William F. Hinson and published by . This book was released on 1962 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Jet Pluming on the Static Stability of Cone-cylinder-fare Configurations at a Mach Number of 9.65 by : William F. Hinson
Download or read book Effect of Jet Pluming on the Static Stability of Cone-cylinder-fare Configurations at a Mach Number of 9.65 written by William F. Hinson and published by . This book was released on 1962 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5 by : D. J. Spring
Download or read book The Static Stability Characteristics of Several Cone-cylinder-flare-cylinder Configurations at Mach Numbers 0.4 to 4.5 written by D. J. Spring and published by . This book was released on 1963 with total page 270 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic characteristics of various cone cylinder-flare-skirt configurations were inves tigated between Mach Numbers 0.4 to 4.5. The Reynolds number range for the tests was from 0.5 to 6.0 million per foot. Data are presented in basic form, along with cross plots, to show the effect of changing various body component shapes. (Author).
Book Synopsis Effects of Jet Billowing on Stability of Missile-type Bodies at Mach 3.85 by : Reino J. Salmi
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:
Book Synopsis Damping in Pitch and Static Stability of Blunt Cone-cylinder-flare Models and Manned Reentry Capsule Models for Various Angles of Attack at a Mach Number of 2.91 by :
Download or read book Damping in Pitch and Static Stability of Blunt Cone-cylinder-flare Models and Manned Reentry Capsule Models for Various Angles of Attack at a Mach Number of 2.91 written by and published by . This book was released on 1961 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Reynolds Number on the Stability of a Blunt-nosed Flared Cylinder from Mach 17.6 to 22.2 in Helium by :
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:
Book Synopsis Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 by : Lucille C. Coltrane
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:
Book Synopsis An Investigation of the Static Stability and Drag of Two Cone-cylinder-flare Re-entry Heads at Mach Numbers from 0.4 to 1.8 by : A. Stanbrook
Download or read book An Investigation of the Static Stability and Drag of Two Cone-cylinder-flare Re-entry Heads at Mach Numbers from 0.4 to 1.8 written by A. Stanbrook and published by . This book was released on 1968 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability Investigation of a Blunted Cone and a Blunted Ogive with a Flared Cylinder Afterbody at Mach Numbers from 0.30 to 2.85 by : Lucille C. Coltrane
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 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Exploratory Tests of the Effects of Jet Plumes on the Flow Over Cone-cylinder-flare Bodies by : Ralph A. Falanga
Download or read book Exploratory Tests of the Effects of Jet Plumes on the Flow Over Cone-cylinder-flare Bodies written by Ralph A. Falanga and published by . This book was released on 1962 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: Schlieren photographs were taken of the flow over cone-cylinder-flare bodies to study the extent of boundary-layer separation due to the presence of rocket jet plumes. Tests were made of three cone-cylinder-flare configurations in the Langley 11-inch hypersonic tunnel at a Mach number of 9.65 and in the Langley Unitary Plan wind tunnel at a Mach number of 4.65 with two additional configurations. The stream Reynolds number varied from approximately 317,000 to 582,000 based on model length. The conical flares had half-angles of 7 or 13 degrees and contained one of two test nozzles with a design Mach number of 3.72 or 4.53.
Book Synopsis An Investigation of the Static Stability and Drag of Two Cone-cylinder-flare Re-entry Heads at Mach Numbers from 0.4 To1.8 by A.Stanbrook and M.D.Dobson by : A. Stanbrook
Download or read book An Investigation of the Static Stability and Drag of Two Cone-cylinder-flare Re-entry Heads at Mach Numbers from 0.4 To1.8 by A.Stanbrook and M.D.Dobson written by A. Stanbrook and published by . This book was released on 1968 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 1.47 to 4.62 of Static Aerodynamic Characteristics of Twelve Nose Cones Designed for Supersonic Impact by :
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:
Book Synopsis Some Effects of Fin Plan Form on the Static Stability of Fin-body Combinations at Mach Number 4.06 by : Edward F. Ulmann
Download or read book Some Effects of Fin Plan Form on the Static Stability of Fin-body Combinations at Mach Number 4.06 written by Edward F. Ulmann and published by . This book was released on 1952 with total page 28 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 Damping in Pitch and Static Stability of Supersonic Impact Nose Cones, Short Blunt Subsonic Impact Nose Cones, and Manned Reentry Capsules at Mach Numbers from 1.93 to 3.05 by : Herman S. Fletcher
Download or read book Damping in Pitch and Static Stability of Supersonic Impact Nose Cones, Short Blunt Subsonic Impact Nose Cones, and Manned Reentry Capsules at Mach Numbers from 1.93 to 3.05 written by Herman S. Fletcher and published by . This book was released on 1960 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
