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: 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: 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: John David Anderson
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN: 9781563477805
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 0
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Book Description
This book is the second edition of a successful, self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. Like the first edition, 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. Because of its success, most of the first edition has been carried over to the second edition with the addition of much new material. This second edition has updated figures and data to complement the presentation and discussion of the fundamentals. New to this edition are some educational tools that the author has found successful in previous books: (1) previews of each chapter written in plain language to inform the reader why it is important to read and understand the material in the chapter, to highlight the important aspects, and to whip up the readers interest; (2) design examples scattered throughout the book to illustrate the applic
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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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).
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: John David Anderson
Publisher:
ISBN: 9780071006682
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 690
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Book Description
Author:
Publisher:
ISBN: 9781600861956
Category : Aerodynamics, Hypersonic
Languages : en
Pages :
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Book Description
Author: Wilbur C. Nelson
Publisher: Elsevier
ISBN: 1483223310
Category : Science
Languages : en
Pages : 801
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Book Description
The High Temperature Aspects of Hypersonic Flow is a record of the proceedings of the AGARD-NATO Specialists' Meeting, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genese, Belgium in April 1962. The book contains the papers presented during the meeting that tackled a broad range of topics in the aspects of hypersonic flow. The subjects covered during the meeting include pressure measurements, interference effects, the use of wind tunnels in aircraft development testing, high temperature gas characteristics, boundary layer research, stability and control and the use of rocket vehicles in flight research. Aerospace engineers and aeronautical engineers will find the book invaluable.
Author: Ethirajan Rathakrishnan
Publisher: John Wiley & Sons
ISBN: 1118821890
Category : Technology & Engineering
Languages : en
Pages : 355
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Book Description
This is an introductory level textbook which explains the elements of high temperature and high-speed gas dynamics. written in a clear and easy to follow style, the author covers all the latest developments in the field including basic thermodynamic principles, compressible flow regimes and waves propagation in one volume covers theoretical modeling of High Enthalpy Flows, with particular focus on problems in internal and external gas-dynamic flows, of interest in the fields of rockets propulsion and hypersonic aerodynamics High enthalpy gas dynamics is a compulsory course for aerospace engineering students and this book is a result of over 25 years' teaching by the author accompanying website includes a Solutions Manual for exercises listed at the end of each chapter, plus lecture slides
