Free Delivery Over $100
|
|
|||
|
||||
OverviewHypersonic ?ight and aerothermodynamics are fascinating topics. Design problems and aerothermodynamic phenomena are partly very di?erent for the various kinds of hypersonic ?ight vehicles. These are-and will be in the future-winged and non-winged re-entry vehicles as well as airbreathing cruise and acceleration and also ascent and re-entry vehicles. Both authors of the book worked for almost four decades in hypersonics: at the German aerospace research establishment (DVL/DFVLR, now DLR) to the end of the 1970s, then in industry (MBB/Dasa, now EADS). They were involved in many major technology programs and projects. First, in the early 1970s, the German ART program (Association for Re-Entry Te- nologies), and, in the 1980s, the European (ESA) HERMES project and the .. German Hypersonics Technology (SANGER) program. Then followed, in the 1990s, the Future European Space Transportation Investigations program (FESTIP), the Manned Space Transportationprogram(MSTP) with the - mosphericRe-EntryDemonstrator(ARD), theX-CRVProjectwiththe X-38 vehicle and, later, the German technology programs TETRA (Technologies for Future Space Transportation Systems), ASTRA (Selected Systems and Technologies for Future Space Transportation Systems Applications), and IMENS (Integrated Multidisciplinary Design of Hot Structures for Space - hicles). Research in the 1960s and 1970s placed great emphasis on low-density ?ows, high temperature real gas e?ects in ground-simulation facilities and, already, on discrete numerical computation methods. After the ?rst ?ights of the Space Shuttle Orbiter with its generally very good aerodynamic p- formance, interest in low-density problems diminished. Full Product DetailsAuthor: Ernst Heinrich Hirschel , Claus WeilandPublisher: Springer-Verlag Berlin and Heidelberg GmbH & Co. KG Imprint: Springer-Verlag Berlin and Heidelberg GmbH & Co. K Edition: 2009 ed. Dimensions: Width: 15.50cm , Height: 2.70cm , Length: 23.50cm Weight: 0.801kg ISBN: 9783642442957ISBN 10: 3642442951 Pages: 512 Publication Date: 21 November 2014 Audience: Professional and scholarly , Professional & Vocational Format: Paperback Publisher's Status: Active Availability: Manufactured on demand  We will order this item for you from a manufactured on demand supplier. Table of ContentsShort Introduction to Flight Trajectories for Aerothermodynamicists.- Aerothermodynamic Design Problems of Winged Re-Entry Vehicles.- Aerothermodynamic Design Problems of Winged Airbreathing Vehicles.- Aerothermodynamic Design Problems of Non-Winged Re-Entry Vehicles.- Stabilization, Trim, and Control Devices.- Forces, Moments, Center-of-Pressure, Trim, and Stability in General Formulation.- Multidisciplinary Design Aspects.- The Thermal State of a Hypersonic Vehicle Surface.- The ?eff Approach and Approximate Relations for the Determination of Aerothermodynamic Parameters.- Solution Guide and Solutions of the Problems.ReviewsFrom the reviews: “Both authors have worked for nearly 40 years on a variety of hypersonic projects so their knowledge and expertise are well worth reading about. … This is a book for people who need an answer; for more understanding consult the multitude of references included, but for practitioners this is a most useful contribution to the literature.” (J. L. Stollery, The Aeronautical Journal, August, 2010) From the reviews: Both authors have worked for nearly 40 years on a variety of hypersonic projects so their knowledge and expertise are well worth reading about. ... This is a book for people who need an answer; for more understanding consult the multitude of references included, but for practitioners this is a most useful contribution to the literature. (J. L. Stollery, The Aeronautical Journal, August, 2010) From the reviews: Both authors have worked for nearly 40 years on a variety of hypersonic projects so their knowledge and expertise are well worth reading about. This is a book for people who need an answer; for more understanding consult the multitude of references included, but for practitioners this is a most useful contribution to the literature. (J. L. Stollery, The Aeronautical Journal, August, 2010) Author InformationTab Content 6Author Website:Countries AvailableAll regions |
||||
