The High-Temperature Hypersonic Gasdynamics Facility Estimated Mach Number 6 Through 14 Performance PDF Download
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Author: Paul Czysz
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 116
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Book Description
The High Temperature Gas Dynamics Facility was developed as a result of the Aeronautical Systems Division's effort to extend the state-of the-art in hypersonic aerodynamic simulation. The facility is a hypersonic wind tunnel supplied with high pressure air, heated from a zirconia dioxide pebble heater. The maximum stagnation pressure and temperature is 40 atres and 4700 R, respectively. This facility is one of four of its kind in this hemisphere and the only Air Force facility of its type. This report discusses the modification of the facility to a two foot diameter test section with a Mach number range of 6 through 14 and its expected performance. This facility is scheduled to be operational in the Fall of 1963.
Author: Paul Czysz
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 116
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Book Description
The High Temperature Gas Dynamics Facility was developed as a result of the Aeronautical Systems Division's effort to extend the state-of the-art in hypersonic aerodynamic simulation. The facility is a hypersonic wind tunnel supplied with high pressure air, heated from a zirconia dioxide pebble heater. The maximum stagnation pressure and temperature is 40 atres and 4700 R, respectively. This facility is one of four of its kind in this hemisphere and the only Air Force facility of its type. This report discusses the modification of the facility to a two foot diameter test section with a Mach number range of 6 through 14 and its expected performance. This facility is scheduled to be operational in the Fall of 1963.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1020
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Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 216
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Book Description
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1148
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Book Description
Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 822
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Book Description
Author: John David Anderson
Publisher: AIAA
ISBN: 9781563474590
Category : Science
Languages : en
Pages : 710
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Book Description
This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 42
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Book Description
The High Temperature, Hypersonic Gasdynamics Facility was developed as a result of the efforts of the Aeronautical Systems Division to extend the state-of-the art in hypersonic aerodynamics simulation. The High Temperature Facility is an operational hypersonic wind tunnel supplied by high pressure, heated air from a zirconium oxide pebble heater. The maximum stagnation pressure is 40 atmospheres, and the maximum temperature is 4700 R. The facility is one of four of its kind in this hemisphere and the only Air Force facility of its type. This report describes its operation from August 1961 until May 1962 as a Mach 4 aerodynamic test facility. The successful operation of this facility is a significant achievement in the area of hypersonic aero dynamic testing techniques.
Author: Robert W. Milling
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 44
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Book Description
A high temperature hypersonic gasdynamics facility is described. It was developed from efforts to extend the state of the art in hypersonic aerodynamic simulation. The high temperature facility is an operational hypersonic wind tunnel supplied by high pressure, heated air from a zirconia dioxide pebble heater. The maximum stagnation pressure and temperature is 40 atmospheres and 4500 F respectively. This facility is one of four of its kind in this hemisphere, and the only Air Force facility of its type. This report describes he first six months operation to include some design and development aspects. The successful operation of this facility is a significant achievement in the area of hypersonic aerodynamic testing techniques.
Author: Bernan
Publisher: UN
ISBN: 9789211011616
Category : Business & Economics
Languages : en
Pages : 136
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Book Description
This authoritative and comprehensive publication reviews recent developments in space science, technology, applications, international cooperation and space law. Compiled from reports prepared for the United Nations Committee on the Peaceful Uses of Outer Space, it aims to increase awareness of the benefits that space activities provide to all countries of the world. Chapters cover: space transportation; robotic earth orbital activities; humans in earth orbit; space studies and exploratino; technology advancement; education; global space markets and opportunities; international co-operationand space law.
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318
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Book Description
