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Book Study of Winglets Applied to Biplanes

Download or read book Study of Winglets Applied to Biplanes written by Peter D. Gall and published by . This book was released on 1985 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Study of Winglets and Other Non planar Wing Configurations for Improved Low speed Aerodynamic Efficiency

Download or read book Study of Winglets and Other Non planar Wing Configurations for Improved Low speed Aerodynamic Efficiency written by Aleix Camúñez i Guirao and published by . This book was released on 2019 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: The induced drag is one of the most important sources of aerodynamic drag in an aircraft, and reducing it could mean saving thousands of dollars in fuel per plane and year. For this reason, since the 1970s oil crisis, agencies like NASA and airplane manufacturers have been developing wing-tip devices with the objective to reduce the induced drag. This work presents a discussion of the effects that the most common used wing-tip devices have on an airplane's aerodynamic and structural performance. It is also discussed the effects of a non-planar wing design, which is a relatively new concept design that has not been used in commercial aircrafts yet. The analysis in this work are based on inviscid flow simulations. Since induced drag only depends on the lift distribution over the wing, it can be approximated with inviscid methods and the boundary layer can be neglected.

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 602 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Book Effects of Winglets on the Drag of a Low Aspect Ratio Configuration

Download or read book Effects of Winglets on the Drag of a Low Aspect Ratio Configuration written by Leigh Ann Smith and published by . This book was released on 1996 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Cumulative Index to a Continuing Bibliography on Aeronautical Engineering

Download or read book A Cumulative Index to a Continuing Bibliography on Aeronautical Engineering written by and published by . This book was released on 1986 with total page 554 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Preliminary Study of Effects of Winglets on Wing Flutter

Download or read book Preliminary Study of Effects of Winglets on Wing Flutter written by Robert V. Doggett and published by . This book was released on 1976 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Study of the Influence of Halfdelta Winglets on Wingtip Vortices

Download or read book Study of the Influence of Halfdelta Winglets on Wingtip Vortices written by Ali A. Abtahi and published by . This book was released on 1982 with total page 186 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government Reports Announcements   Index

Download or read book Government Reports Announcements Index written by and published by . This book was released on 1995 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Advanced Aircraft Design

Download or read book Advanced Aircraft Design written by Egbert Torenbeek and published by John Wiley & Sons. This book was released on 2013-07-29 with total page 438 pages. Available in PDF, EPUB and Kindle. Book excerpt: Although the overall appearance of modern airliners has not changed a lot since the introduction of jetliners in the 1950s, their safety, efficiency and environmental friendliness have improved considerably. Main contributors to this have been gas turbine engine technology, advanced materials, computational aerodynamics, advanced structural analysis and on-board systems. Since aircraft design became a highly multidisciplinary activity, the development of multidisciplinary optimization (MDO) has become a popular new discipline. Despite this, the application of MDO during the conceptual design phase is not yet widespread. Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations. Objectives are aerodynamic efficiency, mission fuel, empty weight and maximum takeoff weight. Independent design variables studied include design cruise altitude, wing area and span and thrust or power loading. Principal features of integrated concepts such as the blended wing and body and highly non-planar wings are also covered. The quasi-analytical approach enables designers to compare the results of high-fidelity MDO optimization with lower-fidelity methods which need far less computational effort. Another advantage to this approach is that it can provide answers to “what if” questions rapidly and with little computational cost. Key features: Presents a new fundamental vision on conceptual airplane design optimization Provides an overview of advanced technologies for propulsion and reducing aerodynamic drag Offers insight into the derivation of design sensitivity information Emphasizes design based on first principles Considers pros and cons of innovative configurations Reconsiders optimum cruise performance at transonic Mach numbers Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes advances understanding of the initial optimization of civil airplanes and is a must-have reference for aerospace engineering students, applied researchers, aircraft design engineers and analysts.

Book Applied Wing Theory

Download or read book Applied Wing Theory written by Elliott Gray Reid and published by . This book was released on 1932 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt: