Author :
Publisher :
Page : 106 pages
File Size : 26,96 MB
Release : 1978
Category :
ISBN :
[PDF] Study Of Hypersonic Propulsion Airframe Integration Technology eBook
Study Of Hypersonic Propulsion Airframe Integration Technology Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Study Of Hypersonic Propulsion Airframe Integration Technology book. This book definitely worth reading, it is an incredibly well-written.
A Numerical Study of Hypersonic Propulsion/airframe Integration Problem
Author : J.R. Narayan
Publisher :
Page : pages
File Size : 28,11 MB
Release : 1989
Category :
ISBN :
Hypersonic Vehicles
Author : Giuseppe Pezzella
Publisher : BoD – Books on Demand
Page : 150 pages
File Size : 28,53 MB
Release : 2019-10-02
Category : Science
ISBN : 1839622695
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.
Hypersonic Technology for Military Application
Author : Division on Engineering and Physical Sciences
Publisher : National Academies Press
Page : 112 pages
File Size : 12,96 MB
Release : 1990-02-01
Category : Technology & Engineering
ISBN : 0309042291
Review and Evaluation of the Air Force Hypersonic Technology Program
Author : National Research Council
Publisher : National Academies Press
Page : 76 pages
File Size : 17,4 MB
Release : 1998-09-05
Category : Technology & Engineering
ISBN : 0309061423
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.
Studies of Engine-airframe Integration on Hypersonic Aircraft
Author : P. J. Johnston
Publisher :
Page : 10 pages
File Size : 25,7 MB
Release : 1970
Category : Airframes
ISBN :
Hypersonic Airbreathing Propulsion
Author : William H. Heiser
Publisher : AIAA
Page : 632 pages
File Size : 24,25 MB
Release : 1994
Category : Science
ISBN : 9781563470356
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
Propulsion Airframe Integration Test Techniques for Hypersonic Airbreathing Configurations at NASA Langley Research Center
Author : David W. Witte
Publisher :
Page : pages
File Size : 41,60 MB
Release : 2003
Category :
ISBN :
Airframe Research and Technology for Hypersonic Airbreathing Vehicles
Author :
Publisher :
Page : 16 pages
File Size : 23,56 MB
Release : 2002
Category :
ISBN :
Studies of Airframe-propulsion-system Integration for Mach 6 Cruise Vehicles
Author :
Publisher :
Page : 26 pages
File Size : 26,90 MB
Release : 1967
Category : Aerodynamics, Hypersonic
ISBN :