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Aerodynamic Stability Technology For Maneuverable Missiles Volume I Configuration Aerodynamic Characteristics
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Book Synopsis Aerodynamic Stability Technology for Maneuverable Missiles. Volume I. Configuration Aerodynamic Characteristics by :
Download or read book Aerodynamic Stability Technology for Maneuverable Missiles. Volume I. Configuration Aerodynamic Characteristics written by and published by . This book was released on 1979 with total page 391 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).
Book Synopsis Aerodynamic Stability Technology for Maneuverable Missiles by : Gennaro F. Aiello
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).
Book Synopsis Aerodynamic Stability Technology for Maneuverable Missiles by : Gennaro F. Aiello
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 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: A procedure for estimating the effects of asymmetric lee-side vortices on slender missile configurations with and without tails is developed, using both theoretical and empirical inputs. A computerized model of the procedure which calculates induced side forces, yawing moments, tail forces and rolling moments is presented. Program flow charts, input instructions and sample cases are provided. Comparisons between experiments data and program calculations show acceptable preliminary design level accuracies. (Author).
Book Synopsis Aerodynamic Stability Technology for Maneuverable Missiles. Volume II. Asymmetric Vortex Effects Computer Program by :
Download or read book Aerodynamic Stability Technology for Maneuverable Missiles. Volume II. Asymmetric Vortex Effects Computer Program written by and published by . This book was released on 1979 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: A procedure for estimating the effects of asymmetric lee-side vortices on slender missile configurations with and without tails is developed, using both theoretical and empirical inputs. A computerized model of the procedure which calculates induced side forces, yawing moments, tail forces and rolling moments is presented. Program flow charts, input instructions and sample cases are provided. Comparisons between experiments data and program calculations show acceptable preliminary design level accuracies. (Author).
Download or read book Missile Aerodynamics written by and published by . This book was released on 1974 with total page 356 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Aerodynamic Assessment of Various Missile Configuration Concepts by :
Download or read book An Aerodynamic Assessment of Various Missile Configuration Concepts written by and published by . This book was released on 1983 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Aerodynamic and Static-Stability Analysis of the Hypersonic Applied Research Technology (HART) Missile by :
Download or read book An Aerodynamic and Static-Stability Analysis of the Hypersonic Applied Research Technology (HART) Missile written by and published by . This book was released on 1994 with total page 225 pages. Available in PDF, EPUB and Kindle. Book excerpt: The flow about the complete Hypersonic Applied Research Technology (HART) missile is simulated for inviscid, laminar, and turbulent conditions and Mach numbers from 2 to 6. An explicit, second-order-accurate, flux-difference- splitting, algorithm is implemented and employed to solve the Navier-Stokes equations. The equations are solved using a finite-volume methodology. The aerodynamic and static-stability characteristics are investigated to determine if conventional supersonic missile configurations can be flown at Mach numbers higher than 5. The effects of nosetip blunting and boundary-layer condition are demonstrated. The structure of the flow near the fins is significantly affected by the turbulent transport of momentum in regions of blocked cross flow. Turbulence and the blockage phenomenon cause bleeding around the fin leading edges. Ultimately, this results in lower fin effectiveness and reduced static stability. The aerodynamic characteristics of the HART missile are predicted at Mach numbers beyond the experimental free-flight testing capabilities. The current predictions indicated that the pitching-moment coefficient decreases with increasing Mach number much less than previous numerical computations. The present results also suggest that the clipped-delta-fin configuration is stable beyond Mach 7.
Book Synopsis Aerodynamic Characteristics of a Series of Twin-inlet Air-breathing Missile Configurations. 1: Axisymmetric Inlets at Supersonic Speeds by : Clyde Hayes
Download or read book Aerodynamic Characteristics of a Series of Twin-inlet Air-breathing Missile Configurations. 1: Axisymmetric Inlets at Supersonic Speeds written by Clyde Hayes and published by . This book was released on 1983 with total page 284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Configured Missile Development by : Robert J. Krieger
Download or read book Aerodynamic Configured Missile Development written by Robert J. Krieger and published by . This book was released on 1980 with total page 136 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of a program that investigated aerodynamic configuring as a method of improving long range supersonic cruise and maneuvering missile performance. Non-circular body, lifting body, blended wing body, wing-body and favorable interference concepts were developed and wind tunnel tested. Substantial improvements in cruise range were shown to result from aero configuring.
Book Synopsis Aerodynamic Configured Missile Development by : Robert J. Krieger
Download or read book Aerodynamic Configured Missile Development written by Robert J. Krieger and published by . This book was released on 1980 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents the results of a program that investigated aerodynamic configuring as a method of improving long range supersonic cruise and maneuvering missile performance. Non-circular body, lifting body, blended wing body, wing-body and favorable interference concepts were developed and wind tunnel tested. Substantial improvements in cruise range were shown to result from aero configuring.
Book Synopsis Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Maneuverable Missile with In-line Cruciform Wings and Canard Surfaces by : M. Leroy Spearman
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.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1973 with total page 1102 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Series of Twin-inlet Air-breathing Missile Configurations: Axisymmetric and two-dimensional inlets at subsonic-transonic speeds by : Clyde Hayes
Download or read book Aerodynamic Characteristics of a Series of Twin-inlet Air-breathing Missile Configurations: Axisymmetric and two-dimensional inlets at subsonic-transonic speeds written by Clyde Hayes and published by . This book was released on 1983 with total page 372 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Analysis and Compilation of Missile Aerodynamic Data. Volume 1: Data Presentation and Analysis by : James O. Nichols
Download or read book Analysis and Compilation of Missile Aerodynamic Data. Volume 1: Data Presentation and Analysis written by James O. Nichols and published by . This book was released on 1977 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: This summary document was prepared in order to facilitate dissemination of a large amount of missile aerodynamic data which has recently been declassified. Only summary data are presented in this report, but a list of reference documents provides sources of detailed data. Most of the configurations considered are suitable for highly maneuverable air-to-air or surface to air missiles; however, data for a few air-to-surface, cruise missile, and one projectile configuration are also presented. The Mach number range of the data is from about 0.2 to 4.63; however, data for most configurations cover only a portion of this range. The following aerodynamic characteristics at various Mach numbers and zero angle of attack are presented.
Book Synopsis Aerodynamic Characteristics of a Series of Airbreathing Missile Configurations by : Clyde Hayes
Download or read book Aerodynamic Characteristics of a Series of Airbreathing Missile Configurations written by Clyde Hayes and published by . This book was released on 1981 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt: Due to the interest in the application of airbreathing propulsion to missiles and the lack of a suitable data base, an experimental program has been conducted to contribute to such a data base. The configurations investigated were with twin-inlets, either two-dimensional or axisymmetric, each located at three circumferential locations. The effects of a wing located above the inlets and of tail configuration were investigated. Longitudinal stability and control and lateral-directional stability were included in the data obtained. This paper presents a summary of the program and some of the results obtained. Certain trends of the data, as well as problem areas, are discussed. Due to the large volume of data obtained, a detailed analysis is not presented. (Author).
Book Synopsis Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2.25, 3.0, and 4.0 by : J. T. Best (Jr.)
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.
Book Synopsis Aerodynamic Characteristics of a Series of Twin-inlet Air-breathing Missile Configurations by : Clyde Hayes
Download or read book Aerodynamic Characteristics of a Series of Twin-inlet Air-breathing Missile Configurations written by Clyde Hayes and published by . This book was released on 1983 with total page 300 pages. Available in PDF, EPUB and Kindle. Book excerpt:
