Download or read book Longitudinal Stability and Control Characteristics of an Air to air Missile Configuration at Mach Numbers of 2 30 and 4 60 and Angles of Attack from Minus 45 Deg to 90 Deg written by and published by . This book was released on 1963 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Stability and Control Characteristics at a Mach Number of 2 01 of a Hypersonic Missile Configuration Having All movable Wing and Tail Surfaces written by Ross B. Robinson and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Stability and Control Characteristics of a Generalized Missile Configuration Employing Several Different Bulk Type Control Schemes at a Mach Number of 6 01 written by and published by . This book was released on 1963 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Stability and Control Characteristics of Missile Configurations Having Several Highly Swept Cruciform Fins and Number of Trailing Edge and Fin Tip Controls at Mach Nubmers from 2 21 to 6 01 written by and published by . This book was released on 1961 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Stability and Control Characteristics at Mach Numbers of 2 01 4 65 and 6 8 of Two Hypersonic Missile Configurations One Having Low aspect ratio Cruciform Wings with Trailing edge Flaps and One Having a Flared Afterbody and All movable Cont written by and published by . This book was released on 1959 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Stability and Control Characteristics at a Mach Number of 2 01 of a Hypersonic Missile Configuration Having All movable Wing and Tail Surfaces written by and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Static Longitudinal Stability and Roll Characteristics of a Three stage Missile Configuration at Mach Numbers from 1 77 to 2 87 written by Donald T. Gregory and published by . This book was released on 1959 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Stability and Control Characteristics at Mach Numbers of 2 86 and 6 02 and Angles of Attack Up to 95 Deg of a Lenticular shaped Reentry Vehicle written by and published by . This book was released on 1961 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1981 with total page 612 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Stability and Control Characteristics at a Mach Number of 2 01 of Several Simulated Air launched Ballistic Missiles Having Various Types of Control Surfaces written by Ross B. Robinson and published by . This book was released on 1961 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Longitudinal Stability and Control Characteristics of a Winged and a Flared Hypersonic Missile Configuration with Various Nose Shapes and Flare Modifications at a Mach Number of 2 01 written by 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 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.
Download or read book Investigation of the Static Longitudinal Stability Characteristics of an Air to surface Canard Missile Configuration in the Transonic Mach Number Range written by Gerald L. Hunt and published by . This book was released on 1960 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Static Longitudinal Stability Characteristics of a Model of an Intermediate range Ballistic Missile at Mach Numbers Between 1 57 and 4 65 written by Robert M. Lust and published by . This book was released on 1960 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Stability and Control Characteristics of a Cruciform Missile Model with Delta Wings and Aft Tail Fin Controls written by William A. Corlett and published by . This book was released on 1979 with total page 117 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted to determine the static stability and control characteristics of a cruciform missile configuration with delta wings and aft tail fin controls. The tests were conducted in the Langley Unitary Plan wind tunnel at Mach numbers from 1.60 to 4.63 through an angle-of-attack range of -4 degree to 30 degree. Model roll orientation was varied from 0 degree to 135 degree. The results indicated good longitudinal stability and control characteristics throughout the test Mach number range. Relatively high induced rolling and yawing moments were apparent at asymmetric model roll angles for the lower test Mach numbers; however, sufficient roll and yaw control was available to trim to relatively high angles of attack and lift coefficients. (Author).
Download or read book Aerodynamic Stability Technology for Maneuverable Missiles written by Gennaro F. Aiello and published by . This book was released on 1979 with total page 396 pages. Available in PDF, EPUB and Kindle. Book excerpt: This study developed empirical methods to predict aerodynamic characteristics of body-tail, body-wing-tail and body-strake-tail missile configurations. Methods cover the Mach number range from 0.6 to 3.0. Methods cover the individual body and tail characteristics at angles of attack from 0 to 180 degrees. For winged bodies the methods encompass angles of attack up to about 30 degrees. All mutual interference effects are accounted for, allowing accurate prediction of force and moment coefficients. (Author).
Download or read book Longitudinal Stability and Control Characteristics from a Flight Investigation of a Cruciform Canard Missile Configuration Having an Exposed Wing canard Area Ratio of 16 1 written by Martin T. Moul and published by . This book was released on 1952 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:
