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The Static And Dynamic Stability Derivatives Of A Blunt Half Cone Entry Configuration At Mach Numbers From 070 To 350
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Book Synopsis The Static and Dynamic Stability Derivatives of a Blunt Half-cone Entry Configuration at Mach Numbers from 0.70 to 3.50 by :
Download or read book The Static and Dynamic Stability Derivatives of a Blunt Half-cone Entry Configuration at Mach Numbers from 0.70 to 3.50 written by and published by . This book was released on 1961 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7 by : Ralph W. Holtzclaw
Download or read book Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7 written by Ralph W. Holtzclaw and published by . This book was released on 1962 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low Subsonic Static and Dynamic Stability Characteristics of Two Blunt 120 ̊cone Configurations by : Richard J. Bendura
Download or read book Low Subsonic Static and Dynamic Stability Characteristics of Two Blunt 120 ̊cone Configurations written by Richard J. Bendura and published by . This book was released on 1967 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Performance and Static Stability Characteristics of a Blunt Nosed, Boattailed, 13 Deg Half Cone at Mach Numbers from 0.6 to 5.0 by :
Download or read book Aerodynamic Performance and Static Stability Characteristics of a Blunt Nosed, Boattailed, 13 Deg Half Cone at Mach Numbers from 0.6 to 5.0 written by and published by . This book was released on 1961 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6 by : Michael F. Sarabia
Download or read book Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6 written by Michael F. Sarabia and published by . This book was released on 1960 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Flow Field and Surface Pressures on a Blunt Half-cone Entry Configuration at Mach Numbers of 7.4 and 10.4 by : George H. Holdaway
Download or read book Flow Field and Surface Pressures on a Blunt Half-cone Entry Configuration at Mach Numbers of 7.4 and 10.4 written by George H. Holdaway 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 LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92 by :
Download or read book THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92 written by and published by . This book was released on 1961 with total page 68 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 Deg Half Cone at Mach Numbers to 0.90 by :
Download or read book The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13 Deg Half Cone at Mach Numbers to 0.90 written by and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Two Blunt, Half-cone Wedge Entry Configurations at Mach Numbers from 2.30 to 4.63 by : Gerald V. Foster
Download or read book Aerodynamic Characteristics of Two Blunt, Half-cone Wedge Entry Configurations at Mach Numbers from 2.30 to 4.63 written by Gerald V. Foster and published by . This book was released on 1968 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Characteristics of an Aerodynamic Control System for Use with Blunt Entry Configurations at Mach Numbers of 10.7 and 21.2 in Helium by :
Download or read book Characteristics of an Aerodynamic Control System for Use with Blunt Entry Configurations at Mach Numbers of 10.7 and 21.2 in Helium written by and published by . This book was released on 1965 with total page 42 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 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 Heat-Transfer and Static Stability Tests of A 7.5-deg Blunt Cone with Roughness Elements and Sonic Jets to Promote Boundary-Layer Transition at Mach Number 10 by : D. B. Carver
Download or read book Heat-Transfer and Static Stability Tests of A 7.5-deg Blunt Cone with Roughness Elements and Sonic Jets to Promote Boundary-Layer Transition at Mach Number 10 written by D. B. Carver and published by . This book was released on 1977 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: Aerothermodynamic transition tests were conducted on a 7.5-deg half- angle, blunt cone model to evaluate variations of trip design in promoting boundary-layer transition on a reentry vehicle. Heat-transfer data were obtained using square-shaped roughness elements and sonic jets as boundary-layer trips to determine the effects of (1) trip height, (2) trip spacing, (3) axial trip location, (4) number of rows of trips, (5) staggered trips, and (6) Reynolds number on heat-transfer distributions. Static stability tests were conducted in conjunction with a few selected trip configurations to determine the influence of the boundary-layer trips on the model static stability and axial-force characteristics. The tests were performed at Mach number 10 for angle-of-attack ranges from 0 to 2 deg (heat-transfer data) and from -7.5 to 7.5 deg (static stability data). Free-stream Reynolds number, based on total model length, was varied from 1.5 to 6.2 million. Selected heat-transfer and static stability data are presented to illustrate the effects of configuration variables and Reynolds number.
Book Synopsis Study of the Stability and Drag at Mach Numbers from 4.5 to 13.5 of a Conical Venus-entry Body by : Peter F. Intrieri
Download or read book Study of the Stability and Drag at Mach Numbers from 4.5 to 13.5 of a Conical Venus-entry Body written by Peter F. Intrieri and published by . This book was released on 1965 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal Stability Characteristics of Various Mercury Escape Configurations and of a Proposed Alternate Escape Configuration for Mach Numbers of 0.05 to 9.60 by : Robert P. Smith
Download or read book Static Longitudinal Stability Characteristics of Various Mercury Escape Configurations and of a Proposed Alternate Escape Configuration for Mach Numbers of 0.05 to 9.60 written by Robert P. Smith and published by . This book was released on 1961 with total page 186 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium by : Melvin J. Fohrman
Download or read book Static Aerodynamic Characteristics of a Short Blunt 10 Degree Semivertex Angle Cone at a Mach Number of 15 in Helium written by Melvin J. Fohrman and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Characteristics of a Variable-geometry Entry Vehicle at Mach Numbers from 10.5 to 21.1 in Helium Flow by :
Download or read book Characteristics of a Variable-geometry Entry Vehicle at Mach Numbers from 10.5 to 21.1 in Helium Flow written by and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
