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Aerodynamic Characteristics Of Two Trailblazer Ii Blunted 9 Cone Reentry Bodies At Mach 68 In Air And 212 In Helium
Download Aerodynamic Characteristics Of Two Trailblazer Ii Blunted 9 Cone Reentry Bodies At Mach 68 In Air And 212 In Helium full books in PDF, epub, and Kindle. Read online Aerodynamic Characteristics Of Two Trailblazer Ii Blunted 9 Cone Reentry Bodies At Mach 68 In Air And 212 In Helium ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Book Synopsis Aerodynamic Characteristics of Two Trailblazer II Blunted 9 ̊cone Reentry Bodies at Mach 6.8 in Air and 21.2 in Helium by : Herbert R. Schippell
Download or read book Aerodynamic Characteristics of Two Trailblazer II Blunted 9 ̊cone Reentry Bodies at Mach 6.8 in Air and 21.2 in Helium written by Herbert R. Schippell and published by . This book was released on 1965 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Truncated-cone Lifting Reentry Body at Mach Numbers from 10 to 21 by :
Download or read book Aerodynamic Characteristics of a Truncated-cone Lifting Reentry Body at Mach Numbers from 10 to 21 written by and published by . This book was released on 1963 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 by : George C. Kenyon
Download or read book The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 written by George C. Kenyon and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 by : James F. Campbell
Download or read book Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 by : Clarence A. Brown
Download or read book Static Aerodynamic Characteristics of a Two-stage and a Three-stage Rocket Vehicle at Mach Numbers from 1.47 to 4.63 written by Clarence A. Brown and published by . This book was released on 1962 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4 by :
Download or read book Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4 written by and published by . This book was released on 1963 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 by : Earl D. Knechtel
Download or read book Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 written by Earl D. Knechtel and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.
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 Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86 by : William John Small
Download or read book Aerodynamic Characteristics of a Hypersonic Transport Configuration at Mach 6.86 written by William John Small and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle-type Vehicle at Subsonic Mach Numbers by : Leland Howard Jorgenson
Download or read book Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle-type Vehicle at Subsonic Mach Numbers written by Leland Howard Jorgenson and published by . This book was released on 1972 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static aerodynamic forces and moments were measured to study the effects of Reynolds number and body corner radius on the aerodynamic characteristics of a straight wing space shuttle orbiter at subsonic speeds. A 0.02-scale model was tested at Mach numbers from 0.3 to 0.9 and Reynolds numbers from about 600,000 to 3 million, based on body width. The body alone and the body with its wing and horizontal tail attached were tested at angles of attack from 35 to 75 degrees. The effects of rounding the body corners at the junctures connecting the bottom and sides were investigated for corner radii from 0 to 8.5 percent of the body width. At low subsonic Mach numbers (free stream Mach number approximately equal 0.3) the aerodynamic characteristics are affected significantly by changes in Reynolds number and body corner radius. With increase in Mach number to free stream Mach number = 0.9 the effect of Reynolds number seems to vanish, but a significant effect of body corner radius remains.
Book Synopsis Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 by : Walter P. Nelms
Download or read book Aerodynamic Characteristics of an All-body Hypersonic Aircraft Configuration at Mach Numbers from 0.65 to 10.6 written by Walter P. Nelms and published by . This book was released on 1971 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerodynamic characteristics of a model designed to represent an all body, hypersonic cruise aircraft are presented for Mach numbers from 0.65 to 10.6. The configuration had a delta planform with an elliptic cone forebody and an afterbody of elliptic cross section. Detailed effects of varying angle of attack (-2 to 15 deg), angle of sideslip (-2 to 8 deg), Mach number, and configuration buildup were considered. In addition, the effectiveness of horizontal tail, vertical tail, and canard stabilizing and control surfaces was investigated. The results indicate that all configurations were longitudinally stable near maximum lift drag ratio. The configurations with vertical tails were directionally stable at all angles of attack. Trim penalties were small at hypersonic speeds for a center of gravity location representative of the airplane, but because of the large rearward travel of the aerodynamic center, trim penalties were severe at transonic Mach numbers.
Book Synopsis Static Longitudinal Aerodynamic Characteristics at a Mach Number of 10.03 of Low-aspect-ratio Wing-body Configurations Suitable for Reentry by : Lawrence Elwood Putnam
Download or read book Static Longitudinal Aerodynamic Characteristics at a Mach Number of 10.03 of Low-aspect-ratio Wing-body Configurations Suitable for Reentry written by Lawrence Elwood Putnam and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Aerodynamic Characteristics of the Ames M-2 Lifting Entry Configuration by :
Download or read book Hypersonic Aerodynamic Characteristics of the Ames M-2 Lifting Entry Configuration written by and published by . This book was released on 1966 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Hypersonic Aerodynamic Characteristics of Four Series of Blunt Lifting Body and Winged Reentry Configurations by :
Download or read book Hypersonic Aerodynamic Characteristics of Four Series of Blunt Lifting Body and Winged Reentry Configurations written by and published by . This book was released on 1964 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Aerodynamic Characteristics of Large Angled Cones with Retrorockets by :
Download or read book The Aerodynamic Characteristics of Large Angled Cones with Retrorockets written by and published by . This book was released on 1970 with total page 238 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Longitudinal Aerodynamic Characteristics of Five Cone Cylinder Flare Bodies of Revolution by :
Download or read book Transonic Longitudinal Aerodynamic Characteristics of Five Cone Cylinder Flare Bodies of Revolution written by and published by . This book was released on 1964 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low Speed Aerodynamic Characteristics of a Modified Blunt 13 Deg Half-cone Lifting-body Configuration Having Deployable Horizontal Tails with Or Without Variable-sweep Wings by :
Download or read book Low Speed Aerodynamic Characteristics of a Modified Blunt 13 Deg Half-cone Lifting-body Configuration Having Deployable Horizontal Tails with Or Without Variable-sweep Wings written by and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
