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Aerodynamic Stability Technology For Maneuverable Missiles
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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. 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. 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).
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 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 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.
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 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 An Aerodynamic and Static-stability Analysis of the Hypersonic Applied Research Technology (HART) Missile by : Kenneth J. Moran (CAPT, USAF.)
Download or read book An Aerodynamic and Static-stability Analysis of the Hypersonic Applied Research Technology (HART) Missile written by Kenneth J. Moran (CAPT, USAF.) and published by . This book was released on 1994 with total page 202 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1978 with total page 1018 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Determination of Aerodynamic Stability Coefficients from Rocket Flight Test Data by : A. C. Bustamante
Download or read book The Determination of Aerodynamic Stability Coefficients from Rocket Flight Test Data written by A. C. Bustamante and published by . This book was released on 1961 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method by which aerodynamic stability coefficients can be determined from rocket flight test data, through the use of accelerometer and gyroscope measurements, is presented. This analysis is intended to be used as a program on the 704 IBM computer.
Book Synopsis Application of Nonlinear Aerodynamic Stability Characteristics to Simplify Missile Control and Guidance Systems by : Howard J. Curfman
Download or read book Application of Nonlinear Aerodynamic Stability Characteristics to Simplify Missile Control and Guidance Systems written by Howard J. Curfman and published by . This book was released on 1955 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :Jack Norman Nielsen Publisher :AIAA (American Institute of Aeronautics & Astronautics) ISBN 13 :9780962062902 Total Pages :450 pages Book Rating :4.0/5 (629 download)
Book Synopsis Missile Aerodynamics by : Jack Norman Nielsen
Download or read book Missile Aerodynamics written by Jack Norman Nielsen and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1988-01-01 with total page 450 pages. Available in PDF, EPUB and Kindle. Book excerpt: The similarities between the airplane and the missile extend beyond their flying capabilities, and at higher operational speeds, the configuration distinctions become even less apparent. " Missile Aerodynamics," a classic now available from AIAA and Nielsen Engineering and Research, Inc., combines the best of missile and airplane aerodynamics, drawing extensively from numerous technical papers to present a rational and unified account of the principles behind missile projection. Evaluate the missile versus the airplane in a multitude of areas, from longitudinal acceleration, wing loading, roll and dynamic stability, guidance and navigation, and more. J.N. Nielsen covers every aspect of missile aerodynamics, from the classification of missiles and basic formulas to innovative aerodynamic controls. In one reliable reference, readers will find hundreds of schematics, equations, and tables with practical applications in missile design and engineering. Originally published by Nielsen Engineering and Research, Inc.
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 1986 with total page 850 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Improved Semiempirical Method for Calculating Aerodynamics of Missiles with Noncircular Bodies by : Frankie Gale Moore
Download or read book An Improved Semiempirical Method for Calculating Aerodynamics of Missiles with Noncircular Bodies written by Frankie Gale Moore and published by . This book was released on 1997 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Missiles, Rockets and Satellites: Technology: means and methods by : United States. Department of the Army
Download or read book Missiles, Rockets and Satellites: Technology: means and methods written by United States. Department of the Army and published by . This book was released on 1958 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Maneuverable Missile with Cruiform Wings and In-line Canard Surfaces at Mach Numbers from 0.50 to 4.63 by :
Download or read book Aerodynamic Characteristics of a Maneuverable Missile with Cruiform Wings and In-line Canard Surfaces at Mach Numbers from 0.50 to 4.63 written by and published by . This book was released on 1966 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
