Download or read book Prediction of Supersonic Store Separation Characteristics Volume I Theoretical Methods and Comparisons with Experiment written by and published by . This book was released on 1976 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt: The primary objective of this report is to describe an investigation to develop a method for predicting the separation characteristics of a store released from a supersonic parent aircraft. The present computer program is designed to handle configurations consisting of a wing without dihedral or incidence which is attached to an axisymmetric fuselage. A pylon can be attached to the wing or under the fuselage. In this work, supersonic flow models are described to represent the configuration and special attention is given to the flow field calculation method. It is shown that the basic method utilizing linear, potential flow theory must be corrected for nonlinear effects caused by the shock from the wing leading edge. Experimental results are presented from a wind-tunnel test program designed to provide data to aid in developing and testing the theory. Comparisons between theory and experiment for flow fields, store loading distributions and store forces and moments indicate fair to very good agreement. Recommendations are given for improving the present method.
Download or read book Prediction of Supersonic Store Separation Characteristics Including Fuselage and Stores of Noncircular Cross Section Volume I Theoretical Methods and Comparisons with Experiment written by and published by . This book was released on 1980 with total page 331 pages. Available in PDF, EPUB and Kindle. Book excerpt: The primary objective of this report is to describe an investigation conducted to develope a method for predicting the trajectory of a store separated from an aircraft flying at supersonic speeds. The aircraft model can include a circular or noncircular fuselage, engine inlets, wing, pylon, ejector rack, and circular and noncircular stores. The linear, potential flow methods used to model the aircraft components are described as are nonlinear corrections which are made to position shock waves more accurately. The methods used to calculate the nonuniform flow field, the store forces and moments, and the store trajectory are presented. Comparisons between theory and experiment for flow fields, store loading distributions, store forces and moments, and store trajectories are shown and discussed. (Author).
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 Aerodynamic Prediction Methods RDF 129 written by Joseph Laney Sims and published by . This book was released on 1989 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1981 with total page 212 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Prediction of Supersonic Store Separation Characteristics Volume II Users Manual for the Computer Program written by Frederick K. Goodwin and published by . This book was released on 1976 with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt: Detailed instructions are presented for using a computer program which calculates the six-degree-of-freedom trajectories of external stores which are separated from fighter-bomber type aircraft flying at supersonic speeds. Single store configurations can be handled by the program. The program uses linear potential-flow theory to model the wing and pylon loading and thickness. Three-dimensional line sources and line doublets are used to model the fuselage and store. The program also calculates the trajectory of the store as it separates from the aircraft. This report describes the program, presents instructions for preparing input for the program, describes the output from the program, and presents a sample case. The program draws heavily on an earlier program for subsonic speeds written by the present authors and described in AFFDL-TR-74-130. (Author).
Download or read book A Collection of Technical Papers written by and published by . This book was released on 1981 with total page 1114 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tactical Missile Aerodynamics written by Michael J. Hemsch and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 1992 with total page 774 pages. Available in PDF, EPUB and Kindle. Book excerpt: This two-volume set includes discussions of the physics of the fluid mechanics phenomena associated with tactical missile flight and the full range of prediction methods required to analyze current and future missiles. It's a valuable resource for missile aerodynamicists, designers, and researchers.
Download or read book NASA SP written by and published by . This book was released on 1984 with total page 394 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Engineering written by and published by . This book was released on 1982 with total page 774 pages. Available in PDF, EPUB and Kindle. Book excerpt: A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Download or read book Prediction of Vortex Shedding from Circular and Noncircular Bodies in Supersonic Flow written by M. R. Mendenhall and published by . This book was released on 1984 with total page 204 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book AIAA 26th Aerospace Sciences Meeting written by and published by . This book was released on 1988 with total page 594 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Computer Programs for Calculating Pressure Distributions Including Vortex Effects on Supersonic Monoplane Or Cruciform Wing body tail Combinations with Round Or Elliptical Bodies written by and published by . This book was released on 1979 with total page 640 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamics of Store Integration and Separation written by North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel. Symposium and published by . This book was released on 1996 with total page 306 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Tactical Missile Aerodynamics General topics written by M. R. Mendenhall and published by . This book was released on 1992 with total page 774 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Directory of Computer Software Applications Physics 1970 May 1978 written by United States. National Technical Information Service and published by . This book was released on 1978 with total page 336 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Government Reports Annual Index written by and published by . This book was released on 1975 with total page 882 pages. Available in PDF, EPUB and Kindle. Book excerpt:
