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:
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:
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:
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:
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:
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:
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:
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:
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:
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:
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:
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:
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.
Download or read book 37th AIAA Aerospace Sciences Meeting and Exhibit written by and published by . This book was released on 1999 with total page 598 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1962 with total page 962 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Journal of the Royal Aeronautical Society written by Royal Aeronautical Society and published by . This book was released on 1962 with total page 1164 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.