Download or read book An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers from 3 0 to 6 3 written by Hermilo R. Gloria and published by . This book was released on 1958 with total page 29 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 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of Static Longitudinal Stability and Control Characteristics of a 33 1 3 Scale DR 123 Missile at Mach Numbers 1 61 2 05 and 2 58 written by Marvin Rubinstein and published by . This book was released on 1956 with total page 96 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 An Investigation of the Static Stability and Control Characteristics of Winged and Wingless Interceptor Missile Models written by John M. Swihart and published by . This book was released on 1959 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1963 with total page 1342 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 An Experimental and Theoretical Study of the Aerodynamic Characteristics of Some Generic Missile Concepts at Mach Numbers from 2 to 6 8 written by and published by . This book was released on 1994 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

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 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 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 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 Experimental Static Stability Studies of Several Tactical Missile Configurations at Mach Numbers from 1 76 to 3 01 written by E. Earl Lindsay and published by . This book was released on 1975 with total page 222 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted in the low supersonic Mach number regime to obtain generalized, systematic force and moment data on several tactical missile configurations. Aerodynamic characteristics were determined for a typical missile body and nine body-fin configurations. The aerodynamic loading on each fin was also obtained for the nine fin configurations in a cruciform arrangement at zero deflection. The test was conducted at Mach numbers of 1.76, 2.00, 2.50, and 3.01 and free-stream Reynolds numbers, based on model length, from 8.3 to 14.5 million. The angle-of-attack range was from -1 to 45 deg, and the roll angle range was from 0 to 90 deg. Results are presented to illustrate the effects of fin aspect ratio, planform shape, and planform area on the missile and fin aerodynamic characteristics.

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 Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2 25 3 0 and 4 0 written by J. T. Best (Jr.) and published by . This book was released on 1974 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.

Download or read book A Flight Investigation at Mach Numbers from 0 67 to 1 81 of the Longitudinal Stability and Control Characteristics of a 60 Degree Delta wing Missile Configuration Having an All movable Tail written by Martin T. Moul and published by . This book was released on 1953 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: