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Author : Konstantin Nikolaevich Volkov
Publisher : Unknown
Page : 0 pages
File Size : 55,6 Mb
Release : 2023
Category : Aerodynamics, Hypersonic
ISBN : 1837682607
Author : Anonim
Publisher : Unknown
Page : 590 pages
File Size : 53,5 Mb
Release : 1967
Category : Airplanes
ISBN : STANFORD:36105024706413
Author : F. Edward McLean,Harry W. Carlson,Lynn W. Hunton
Publisher : Unknown
Page : 28 pages
File Size : 46,8 Mb
Release : 1966
Category : Hypersonic planes
ISBN : UIUC:30112106776336
Author : A. Buchanan Barbour,Sir Harold Edward Whittingham
Publisher : Unknown
Page : 620 pages
File Size : 40,6 Mb
Release : 1962
Category : Aviation medicine
ISBN : UOM:39015004441724
Author : Giuseppe Pezzella,Antonio Viviani
Publisher : BoD – Books on Demand
Page : 150 pages
File Size : 49,7 Mb
Release : 2019-10-02
Category : Science
ISBN : 9781839622694
In 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 : North Atlantic Treaty Organization. Research and Technology Organization
Publisher : Unknown
Page : 342 pages
File Size : 45,6 Mb
Release : 1998
Category : Aerodynamics, Supersonic
ISBN : CORNELL:31924084503766
Contains the lecture notes prepared for a Special Course on Fluid Dynamics Research on Supersonic Aircraft organized by the RTO Applied Vehicle Technology Panel (AVT). The Course was held at the von Kármán Institute for Fluid Dynamics (VKI) Institute, Rhode-Saint-Genèse, Belgium 25-29 May 1998. The following topics were covered: History & Economics of Supersonic Transports, Supersonic Aerodynamics, Sonic Boom Theory and Minimization, Multi-Point Design Challenges, Vortex Plume Interactions, Propulsion System Design. Presentations on the major world wide supersonic transport programs were also included. The material assembled in this publication was prepared under the combined sponsorship of the RTO Applied Vehicle Technology Panel, the Consultant and Exchange Program of RTO, and the von Kármán Institute (VKI) for Fluid Dynamics.
Author : T. A. Heppenheimer
Publisher : Unknown
Page : 364 pages
File Size : 42,6 Mb
Release : 2006
Category : Science
ISBN : PURD:32754079096438
Hypersonics is the study of flight at speeds where aerodynamic heating dominates the physics of the problem. Typically this is Mach 5 and higher. Hypersonics is an engineering science with close links to supersonics and engine design. Within this field, many of the most important results have been experimental. The principal facilities have been wind tunnels and related devices, which have produced flows with speeds up to orbital velocity. Why is it important? Hypersonics has had two major applications. The first has been to provide thermal protection during atmospheric entry. Success in this enterprise has supported ballistic-missile nose cones, has returned strategic reconnaissance photos from orbit and astronauts from the Moon, and has even dropped an instrument package into the atmosphere of Jupiter. The last of these approached Jupiter at four times the speed of a lunar mission returning to Earth. Work with re-entry has advanced rapidly because of its obvious importance. The second application has involved high-speed propulsion and has sought to develop the scramjet as an advanced airbreathing ramjet. Scramjets are built to run cool and thereby to achieve near-orbital speeds. They were important during the Strategic Defense Initiative, when a set of these engines was to power the experimental X-30 as a major new launch vehicle. This effort fell short, but the X-43A, carrying a scramjet, has recently flown at Mach 9.65 by using a rocket. Atmospheric entry today is fully mature as an engineering discipline. Still, the Jupiter experience shows that work with its applications continues to reach for new achievements. Studies of scramjets, by contrast, still seek full success, in which such engines can accelerate a vehicle without the use of rockets. Hence, there is much to do in this area as well. For instance, work with computers may soon show just how good scramjets can become. NASA SP-2007-4232
Author : National Research Council,Division on Engineering and Physical Sciences,Aeronautics and Space Engineering Board,Committee on Breakthrough Technology for Commercial Supersonic Aircraft
Publisher : National Academies Press
Page : 128 pages
File Size : 46,6 Mb
Release : 2002-02-16
Category : Technology & Engineering
ISBN : 9780309082778
High-speed flight is a major technological challenge for both commercial and business aviation. As a first step in revitalizing efforts by the National Aeronautics and Space Administration (NASA) to achieve the technology objective of high-speed air travel, NASA requested the National Research Council (NRC) to conduct a study that would identify approaches for achieving breakthroughs in research and technology for commercial supersonic aircraft. Commercial Supersonic Technology documents the results of that effort. This report describes technical areas where ongoing work should be continued and new focused research initiated to enable operational deployment of an environmentally acceptable, economically viable commercial aircraft capable of sustained supersonic flight, including flight over land, at speeds up to approximately Mach 2 in the next 25 years or less.
Author : National Research Council,Division on Engineering and Physical Sciences,Commission on Engineering and Technical Systems,Committee on Review and Evaluation of the Air Force Hypersonic Technology Program
Publisher : National Academies Press
Page : 76 pages
File Size : 49,7 Mb
Release : 1998-09-05
Category : Technology & Engineering
ISBN : 9780309061421
This study was undertaken in response to a request by the U.S. Air Force that the National Research Council (NRC) examine whether the technologies that underlie the concept of a hypersonic, air-launched, air-breathing, hydrocarbon-fueled missile with speeds up to Mach 81 can be demonstrated in time to be initially operational by 2015. To conduct the study, the NRC appointed the Committee on Review and Evaluation of the Air Force Hypersonic Technology Program, under the auspices of the Air Force Science and Technology Board.
Author : Lawrence W. Reithmaier
Publisher : McGraw Hill Professional
Page : 296 pages
File Size : 44,8 Mb
Release : 1995
Category : Science
ISBN : 0070520216
Publisher's Note: Products purchased from Third Party sellers are not guaranteed by the publisher for quality, authenticity, or access to any online entitlements included with the product. This compelling book opens up the world of high-speed flight to readers who do not have extensive technical backgrounds Covering both subsonic and supersonic flight, it demystifies the world of high-speed aerodynamics, flight principles, gas turbine jets, and more. You'll learn why there are no supersonic airliners, what problems confront designers of 2,000-mph aircraft, and whether or not a hypersonic, or Mach 5, airplane is likely to be built.
Author : United States. Congress. Senate. Committee on Commerce. Aviation Subcommittee
Publisher : Unknown
Page : 544 pages
File Size : 47,7 Mb
Release : 1963
Category : Aeronautics and state
ISBN : UIUC:30112121383035
Author : Giuseppe Pezzella,Antonio Viviani
Publisher : BoD – Books on Demand
Page : 132 pages
File Size : 44,5 Mb
Release : 2022-05-04
Category : Science
ISBN : 9781839699320
Some sixty years after the experimental flights of the North American X-15 hypersonic rocket-powered aircraft, sustained hypervelocity travel is still the next frontier in high-speed transportation. Today, there is much excitement and interest regarding hypersonic vehicles. In fact, many aerospace agencies, large industries, and several start-ups are involved in design activities and experimental campaigns both in wind tunnels and in-flight with full-scale experimental flying test beds and prototypes to make hypersonic travel almost as easy and convenient as airliner travel. Achieving this goal will radically revolutionize the future of civil transportation. This book contains valuable contributions that focus on various design issues related to hypersonic aircraft.
Author : United States. Congress. House. Committee on Appropriations
Publisher : Unknown
Page : 1216 pages
File Size : 43,9 Mb
Release : 1963
Category : Electronic
ISBN : MINN:31951D03538353D
Author : William H. Heiser,David T. Pratt
Publisher : AIAA
Page : 632 pages
File Size : 54,8 Mb
Release : 1994
Category : Science
ISBN : 1563470357
An almost entirely self-contained engineering textbook primarily for use in undergraduate and graduate courses in airbreathing propulsion. It provides a broad and basic introduction to the elements needed to work in the field as it develops and grows. Homework problems are provided for almost every individual subject. An extensive array of PC-based user-friendly computer programs is provided in order to facilitate repetitious and/or complex calculations. Annotation copyright by Book News, Inc., Portland, OR
Author : United States. Congress. House. Committee on Appropriations. Subcommittee on Independent Offices
Publisher : Unknown
Page : 1224 pages
File Size : 48,5 Mb
Release : 1963
Category : Executive departments
ISBN : MINN:31951P011806464