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Author : I. SHANTZ
Publisher :
ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.:/5 (227 download)
Download or read book Dynamic Wind-tunnel Tests of a Fin-stabilized Projectile written by I. SHANTZ and published by . This book was released on 1957 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.F/5 ( download)
Download or read book Design for Control of Projectile Flight Characteristics written by and published by . This book was released on 1966 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : T. M. CLANCY
Publisher :
ISBN 13 :
Total Pages : 15 pages
Book Rating : 4.:/5 (227 download)
Download or read book Wind-tunnel Investigation of the Body of a Fin-stabilized, Discarding-sabot Projectile written by T. M. CLANCY and published by . This book was released on 1952 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.:/5 (932 download)
Download or read book Wind Tunnel Tests on Blunt Body Explosively Formed Projectile written by and published by . This book was released on 1995 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt: Describes supersonic wind tunnel tests in a 0.6-by-0.6-metre indraft facility to study the flight dynamic stability of a particular explosively-formed projectile configuration named Blunt Body. The tests were intended to gather experimental data on surface static pressure distribution and aerodynamic stability coefficients. Results are presented for tests made with a 6-blunt-fin explosively-formed projectile model. The model configuration was obtained from high-speed photography of various real projectiles in flight. A total of 107 runs were made at Mach numbers of 2.97, 3.50, and 3.99, for a variety of roll angles and angles of attack up to 15 degrees. Equations used for data treatment are included as well as a description of the instrumentation test setting and several model drawings. Comparisons are also made to results of computational fluid dynamics simulations.
Author :
Publisher :
ISBN 13 :
Total Pages : 716 pages
Book Rating : 4.:/5 (59 download)
Download or read book On the Accuracy of Flechettes by Dynamic Wind Tunnel Tests, by Theory and Analysis, and by Actual Firings written by and published by . This book was released on 1975 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : William G. Reinecke
Publisher : CRC Press
ISBN 13 : 9781566769013
Total Pages : 2108 pages
Book Rating : 4.7/5 (69 download)
Download or read book Ballistics 18th International Symposium written by William G. Reinecke and published by CRC Press. This book was released on 1999-11-10 with total page 2108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 456 pages
Book Rating : 4.:/5 (31 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 456 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author : C. A. Brebbia
Publisher : WIT Press
ISBN 13 : 1845640772
Total Pages : 257 pages
Book Rating : 4.8/5 (456 download)
Download or read book Computational Ballistics III written by C. A. Brebbia and published by WIT Press. This book was released on 2007 with total page 257 pages. Available in PDF, EPUB and Kindle. Book excerpt: Containing the proceedings of the Third International Conference on Computational Ballistics, this book presents new ideas and advanced developments in the field of study of Computational Ballistics. Ballistic studies include applications as varied as the study of the structural and control behavior of rockets and communication satellites; bird strike effects on commercial aircraft, terrorist attacks and automobile crack worthiness modelling. Many basic problems of ballistics are similar to those in other fields of applications, such as combustion, heat conduction, in-flight structural behaviour, trajectory related issues, contact, impact, penetration, structural response to shock waves and many others.A valuable contribution to its field, this text will be of interest to researchers involved in the different areas of computational ballistics and their relationship between computational methods and experiments. Notable topics include: Systems and Technolog; Combustion and Heat Transfer; Propellants; Fluid Dynamics; Fluid Flow and Aerodynamics; In-Flight Structural Behaviour and Material Response; Guidance and Control; Perforation and Penetration Mechanics; Fluid-structure Interaction; Experimental Mechanics/ballistic and Field Testing; High Rate Loads; Composite Material; Shock and Impact.
Author : Richmond P. Boyden
Publisher :
ISBN 13 :
Total Pages : 86 pages
Book Rating : 4.:/5 (31 download)
Download or read book Transonic Static and Dynamic Stability Characteristics of a Finned Projectile Configuration written by Richmond P. Boyden and published by . This book was released on 1978 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. E. Dillon
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Flight Dynamics of Fin-stabilized Projectiles written by R. E. Dillon and published by . This book was released on 1996 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (227 download)
Download or read book Wind-Tunnel Test of a Spinning, Low-Drag Projectile with Canted Bore Riders at Mach Numbers from 1.75 to 2.5 written by and published by . This book was released on 1974 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Test data are reported for a spin-stabilized, low-drag projectile with and without bore riders mounted at various angles of cant with respect to the shell axis. Wind-tunnel tests were performed with and without spin at four Mach numbers evenly spaced from 1.75 to 2.5; some of the resulting aerodynamic coefficients are plotted versus spin rate, angle of attack or Mach number. (Author).
Author : Klaus O. Opalka
Publisher :
ISBN 13 :
Total Pages : 81 pages
Book Rating : 4.:/5 (227 download)
Download or read book Wind-Tunnel Test of a Spinning, Low-Drag Projectile with Canted Bore Riders at Mach Numbers from 1.75 to 2.5 written by Klaus O. Opalka and published by . This book was released on 1974 with total page 81 pages. Available in PDF, EPUB and Kindle. Book excerpt: Test data are reported for a spin-stabilized, low-drag projectile with and without bore riders mounted at various angles of cant with respect to the shell axis. Wind-tunnel tests were performed with and without spin at four Mach numbers evenly spaced from 1.75 to 2.5; some of the resulting aerodynamic coefficients are plotted versus spin rate, angle of attack or Mach number. (Author).
Author : United States. Army Materiel Command
Publisher :
ISBN 13 :
Total Pages : 290 pages
Book Rating : 4.3/5 (91 download)
Download or read book Design for Control of Projectile Flight Characteristics written by United States. Army Materiel Command and published by . This book was released on 1966 with total page 290 pages. Available in PDF, EPUB and Kindle. Book excerpt: This handbook presents a general survey of the principal factors affecting the flight of projectiles, and describes the methods commonly used for predicting and influencing the flight performance. The coefficients which characterize the aerodynamic forces and moments of a moving body are identified, methods for determining the coefficients applicable to a projectile having a given shape and center of gravity location are described, and the coefficients of a number of projectiles and projectile shapes are given. The use of aerodynamic coefficients in predicting stability, range and accuracy is described. The effects of variations in projectile shape and center of gravity location on range, accuracy and lethality are discussed. Some material on prototype testing and the effects of round-to-round variations in production lots is presented.
Author : L. C. MacAllister
Publisher :
ISBN 13 :
Total Pages : 67 pages
Book Rating : 4.:/5 (227 download)
Download or read book The Effect of a Sub-Caliber Cylindrical After-body on the Behavior of Spin-Stabilized Projectiles written by L. C. MacAllister and published by . This book was released on 1975 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt: Range, wind tunnel, and instrumented free-flight tests have shown that a subcaliber boom at the base of a spin-stabilized projectile will produce significant changes at both small and large yaws. Almost all properties, but in particular the static and magnus moments, are affected. These aerodynamic changes, together with the inertial properties of the shell, are shown to affect both the static and the dynamic stability adversely. (Author).
Author : W. Liess
Publisher :
ISBN 13 :
Total Pages : 9 pages
Book Rating : 4.:/5 (761 download)
Download or read book Calculation of the Stability of a Spin-free-elongated Projectile written by W. Liess and published by . This book was released on 1948 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: Supersonic wind-tunnel tests were conducted at Mach numbers 2.8 and 3.2 on a fin-stabilized elongated projectile, to determine the possibility of increasing the length of the projectile from 19 to 25 calibers in order to increase the explosive charge of the projectile without jeopardizing stability. A 10-caliber long projectile had been successfully tested by firing. Fin effectiveness was reduced slightly by thickening of the boundary layer near the real of the elongated projectile. The question of structural strength caused by elongation is not discussed.
Download or read book Concordantia in Valerii Flacci Argonautica written by and published by . This book was released on 1988 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : D. M. Orchard
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Wind Tunnel Tests on the H3P78, Power Law Elliptic Section Flared Projectile from Mach 2.5 to 4.0 written by D. M. Orchard and published by . This book was released on 2001 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
