Download or read book Effects of Canard Location on the Aerodynamic Characteristics of a Sharp nosed Missile at Mach Numbers of 1 5 and 2 0 written by and published by . This book was released on 1977 with total page 742 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Canard Location on the Aerodynamic Characteristics of a Blunt nosed Missile at Mach Numbers of 1 5 and 2 0 written by Donald L. Kassner and published by . This book was released on 1977 with total page 292 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental Investigation of the Aerodynamic Characteristics of Nose Mounted Canard Configurations at Supersonic Mach Numbers 1 5 Through 4 5 written by James R Burt (Jr.) and published by . This book was released on 1976 with total page 352 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted in a supersonic wind tunnel to determine the aerodynamic characteristics of several nose mounted canard wing configurations. Canard position, geometry, angular orientation, and model nose shape were varied systematically to determine their effects on model aerodynamics. The model was tested at angles of attack of -5 to 13 degrees and Mach numbers of 1.5 to 4.5. Aerodynamic loads were measured separately on four canards and tail panels, and the total model. The vapor screen method was used to trace the paths of the vortices shed from the canards. Roll control effectiveness of canards, both with a planar tail and a ring tail was investigated.

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Preliminary Investigation of the Effects of Several Seeker nose Configurations on the Longitudinal Characteristics of a Canard type Missile at a Mach Number of 1 60 written by A. Warner Robins and published by . This book was released on 1958 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Characteristics of a Canard controlled Missile at Mach Numbers of 0 8 1 3 and 1 75 written by and published by . This book was released on 1977 with total page 262 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Characteristics at Mach Numbers from 1 50 to 4 63 of a Maneuverable Missile with In line Cruciform Wings and Canard Surfaces written by M. Leroy Spearman and published by . This book was released on 1967 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley Unitary Plan wind tunnel at Mach numbers from 1.50 to 4.63 to determine the aerodynamic characteristics of a maneuverable missile having in-line cruciform wings and canard surfaces oriented in 45° roll planes.

Download or read book Aerodynamic Characteristics of a Canard controlled Missile at Mach Numbers of 1 5 and 2 0 written by Donald L. Kassner and published by . This book was released on 1977 with total page 296 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book An Experimental Investigation of the Aerodynamic Characteristics of Several Nose mounted Canard Configurations at Transonic Mach Numbers written by James R Burt (Jr.) and published by . This book was released on 1974 with total page 778 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted at the CALSPAN Corporation's transonic wind tunnel to determine the aerodynamic characteristics of several nose-mounted canard wing configurations. Canard position, geometry, angular orientation, and model nose shape were varied systematically to determine their effects on model aerodynamics. Angle of attack was varied from -3 to 12 degrees and Mach number was varied from 0.6 to 1.25. Aerodynamic loads were measured separately for each of the four canards and tail surfaces, and the total model.

Download or read book Aerodynamic Characteristics at Mach Numbers from 1 60 to 2 16 of a Blunt nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins written by William J. Monta and published by . This book was released on 1971 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Characteristics in Pitch of a Series of Cruciform wing Missiles with Canard Controls at a Mach Number of 2 01 written by M. Leroy Spearman 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 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 Effect of Tail fin Span on Stability and Control Characteristics of a Canard controlled Missile at Supersonic Mach Numbers written by A. B. Jr Blair and published by . This book was released on 1983 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect on Tail fin Span on Stability and Control Characteristics of a Canard controlled Missile at Supersonic Mach Numbers written by A. B. Blair and published by . This book was released on 1983 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Characteristics at Mach Numbers from 0 60 to 1 16 of a Canard Configuration Designed for Supersonic Cruise Flight written by and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Nose Bluntness on Aerodynamic Characteristics of Cruciform finned Missile Configuration at Mach 1 50 to 2 86 written by Lloyd S. Jernell and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Numerical Investigation of Aerodynamics of Canard controlled Missile Using Planar and Grid Tail Fins written by James DeSpirito and published by . This book was released on 2004 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt: Viscous computational fluid dynamic simulations were used to predict the aerodynamic coefficients and flow field around a canard-controlled missile in subsonic and transonic flow. Computations were performed at Mach 0.6 and 0.9, six angles of attack between 0 deg and 10 deg, and with planar and grid tail fins. The computations were validated with wind tunnel data. Flow visualizations showed that the canard downwash produced a low-pressure region on the starboard side of the missile that produced a large induced side force. The canard trailing vortices interacted with the tail fins until alpha> 8 deg, producing a pressure differential on the leeward tail fin, leading to the adverse induced roll effects. Visualizations of the flow through the grid fin structure showed choking of the flow at Mach 0.9 and Mach 1.5. The validated simulations results showed that grid fins did not improve the canard roll-control effectiveness at subsonic and transonic speeds as well as they did at the low supersonic speed.