A Study Of Various Slender And Non Slender Fin Body Combinations Of Missile Configurations
DOWNLOAD
FREE 30 Days
Download A Study Of Various Slender And Non Slender Fin Body Combinations Of Missile Configurations PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get A Study Of Various Slender And Non Slender Fin Body Combinations Of Missile Configurations book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages. If the content not found or just blank you must refresh this page
A Study Of Various Slender And Non Slender Fin Body Combinations Of Missile Configurations
DOWNLOAD
FREE 30 Days
Author : N. Uchiyama
language : en
Publisher:
Release Date : 1976
A Study Of Various Slender And Non Slender Fin Body Combinations Of Missile Configurations written by N. Uchiyama and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Aerodynamic load categories.
The aerodynamic loading on a number of rocket body-control surface combinations has been calculated using methods developed at the University of Tennessee Space Institute over the past five years. Variations in control surface planform, roll angle, control surface deflection or incorporation of elevons, are included. Compressibility is accounted for. Details of the digital computer program are included.
Missile Dynamics Equations For Guidance And Control Modeling And Analysis
DOWNLOAD
FREE 30 Days
Author : Philip N. Jenkins
language : en
Publisher:
Release Date : 1976
Missile Dynamics Equations For Guidance And Control Modeling And Analysis written by Philip N. Jenkins and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1976 with Equations of motion categories.
This report documents some techniques used in deriving the equations of motion of a missile for a six-degree-of-freedom (6-DOF) simulation. Several forms of the equations are developed, and their implementation is discussed. Specific emphasis is placed on showing the interrelation of the equation forms currently in use by showing their development from the basic laws. This report is meant to serve as a primer for new engineers and as a reference for all engineers involved in missile flight simulation.
Scientific And Technical Aerospace Reports
DOWNLOAD
FREE 30 Days
Author :
language : en
Publisher:
Release Date : 1995
Scientific And Technical Aerospace Reports written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1995 with Aeronautics categories.
Proceedings
DOWNLOAD
FREE 30 Days
Author :
language : en
Publisher:
Release Date : 1977
Proceedings written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977 with Astronautics categories.
Parametric Fin Body And Fin Plate Database For A Series Of 12 Missile Fins
DOWNLOAD
FREE 30 Days
Author : Jerry M. Allen
language : en
Publisher:
Release Date : 2001
Parametric Fin Body And Fin Plate Database For A Series Of 12 Missile Fins written by Jerry M. Allen and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 2001 with Aerodynamic measurements categories.
A cooperative experimental investigation has been performed to obtain a systematic fin-body and fin-plate database for series of 12 missile fins. These data are intended to complement and extend the information contained in the Triservice missile project and to provide a systematic set of experimental data from which fin-body interference factors can be derived. Data were obtained with the fins mounted on both an axisymmetric body and on a flat plate that was used to simulate fin-alone measurements. The experiments were conducted at Mach numbers from 0.60 to 3.95; fin deflection angles of 0°, 10° , and -10° ; and angles of attack up to 30° on the body and up to 95° on the flat plate. The data were obtained from three-component balances attached to the fins and a six-component balance located in the axisymmetric body. The data obtained in this project are documented in tabular form in this report. In addition, selected data are presented in graphical form to illustrate the effects of the test variables.
Government Reports Annual Index
DOWNLOAD
FREE 30 Days
Author :
language : en
Publisher:
Release Date : 1982
Government Reports Annual Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1982 with Government reports announcements & index categories.
Technical Information Pilot
DOWNLOAD
FREE 30 Days
Author :
language : en
Publisher:
Release Date : 1952
Technical Information Pilot written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1952 with Science categories.
Government Reports Announcements Index
DOWNLOAD
FREE 30 Days
Author :
language : en
Publisher:
Release Date : 1977-03
Government Reports Announcements Index written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1977-03 with Science categories.
Wind Tunnel Investigation Of A Number Of Total Pressure Tubes At High Angles Of Attack
DOWNLOAD
FREE 30 Days
Author : A. Gerald Rainey
language : en
Publisher:
Release Date : 1957
Wind Tunnel Investigation Of A Number Of Total Pressure Tubes At High Angles Of Attack written by A. Gerald Rainey and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aerodynamics categories.
Report
DOWNLOAD
FREE 30 Days
Author :
language : en
Publisher:
Release Date : 1957
Report written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1957 with Aeronautics categories.