Papers Presented at the AIAA Fourth International Aerospace Planes Conference
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Published: 1992
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Published: 1992
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Published: 1992
Total Pages: 476
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Published: 1992
Total Pages: 414
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DOWNLOAD EBOOKAuthor: American Institute of Aeronautics and Astronautics
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Published: 1992
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Published: 1991
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Published: 1992
Total Pages: 488
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Published: 1990
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DOWNLOAD EBOOKAuthor: American Institute of Aeronautics and Astronautics
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Published: 1991
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DOWNLOAD EBOOKAuthor: Giuseppe Pezzella
Publisher: BoD – Books on Demand
Published: 2019-10-02
Total Pages: 150
ISBN-13: 1839622695
DOWNLOAD EBOOKIn the aviation field there is great interest in high-speed vehicle design. Hypersonic vehicles represent the next frontier of passenger transportation to and from space. However, several design issues must be addressed, including vehicle aerodynamics and aerothermodynamics, aeroshape design optimization, aerodynamic heating, boundary layer transition, and so on. This book contains valuable contributions focusing on hypervelocity aircraft design. Topics covered include hypersonic aircraft aerodynamic and aerothermodynamic design, especially aeroshape design optimization, computational fluid dynamics, and scramjet propulsion. The book also discusses high-speed flow issues and the challenges to achieving the dream of affordable hypersonic travel. It is hoped that the information contained herein will allow for the development of safe and efficient hypersonic vehicles.
Author: Paul A. Czysz
Publisher: Springer
Published: 2017-08-30
Total Pages: 515
ISBN-13: 3662547449
DOWNLOAD EBOOKThe updated and expanded third edition of this book focuses on the multi-disciplinary coupling between flight-vehicle hardware alternatives and enabling propulsion systems. It discusses how to match near-term and far-term aerospace vehicles to missions and provides a comprehensive overview of the subject, directly contributing to the next-generation space infrastructure, from space tourism to space exploration. This holistic treatment defines a mission portfolio addressing near-term to long-term space transportation needs covering sub-orbital, orbital and escape flight profiles. In this context, a vehicle configuration classification is introduced covering alternatives starting from the dawn of space access. A best-practice parametric sizing approach is introduced to correctly design the flight vehicle for the mission. This technique balances required mission with the available vehicle solution space and is an essential capability sought after by technology forecasters and strategic planners alike.