Experimental Pressure Distributions Over Blunt Two- and Three-dimensional Bodies Having Similar Cross Sections at a Mach Number of 4.95 PDF Download

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Experimental Pressure Distributions Over Blunt Two- and Three-dimensional Bodies Having Similar Cross Sections at a Mach Number of 4.95

Experimental Pressure Distributions Over Blunt Two- and Three-dimensional Bodies Having Similar Cross Sections at a Mach Number of 4.95 PDF Author: Jerome D. Julius
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

Book Description


Experimental Pressure Distributions Over Blunt Two- and Three-dimensional Bodies Having Similar Cross Sections at a Mach Number of 4.95

Experimental Pressure Distributions Over Blunt Two- and Three-dimensional Bodies Having Similar Cross Sections at a Mach Number of 4.95 PDF Author: Jerome D. Julius
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

Book Description


An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow

An Experimental Study of the Pressure and Heat-transfer Distribution on a 70° Sweep Slab Delta Wing in Hypersonic Flow PDF Author: Mitchel H. Bertram
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 136

Book Description
Results are presented for a study of the pressure and heat-transfer distributions and force characteristics of slab delta wings of 70° sweep at Mach numbers of 6.8 and 9.6 in air and 18 in helium. The wings had cylindrical leading edges and were tested with two different noses. One was sharp in plan view and the other was a tangent sphere with the same diameter as the cylindrical leading edge. Simple approaches to predicting the heat transfer are shown to be successful if the flow pattern peculiar to the angle-of-attack range under consideration is taken into account.

NASA Technical Report

NASA Technical Report PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 930

Book Description


NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 548

Book Description


Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 686

Book Description


Hypersonic and High Temperature Gas Dynamics

Hypersonic and High Temperature Gas Dynamics PDF Author: John David Anderson
Publisher: AIAA
ISBN: 9781563474590
Category : Science
Languages : en
Pages : 710

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.

Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 712

Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1492

Book Description


Experimental Pressure Distribution on an Asymmetrical Nonconical Body at a Mach Number 1.90

Experimental Pressure Distribution on an Asymmetrical Nonconical Body at a Mach Number 1.90 PDF Author: DeMarquis D. Wyatt
Publisher:
ISBN:
Category :
Languages : en
Pages : 58

Book Description


U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 188

Book Description