Supersonic Flow Past a Family of Blunt Axisymmetric Bodies PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Supersonic Flow Past a Family of Blunt Axisymmetric Bodies PDF full book. Access full book title Supersonic Flow Past a Family of Blunt Axisymmetric Bodies by Milton Van Dyke. Download full books in PDF and EPUB format.
Author: Milton Van Dyke
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Get Book Here
Book Description
Some 100 numerical computations have been carried out for unyawed bodies of revolution with detached bow waves. The gas is assumed perfect with y=5/3, 7/5, or 1. Free-stream Mach numbers are taken as 1.2, 1.5, 2, 3, 4, 6, 10, and [infinity symbol]. The results are summarized with emphasis on the sphere and paraboloid.
Author: Milton Van Dyke
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Get Book Here
Book Description
Some 100 numerical computations have been carried out for unyawed bodies of revolution with detached bow waves. The gas is assumed perfect with y=5/3, 7/5, or 1. Free-stream Mach numbers are taken as 1.2, 1.5, 2, 3, 4, 6, 10, and [infinity symbol]. The results are summarized with emphasis on the sphere and paraboloid.
Author: Benjamin R. Briggs
Publisher:
ISBN:
Category : Numerical analysis
Languages : en
Pages : 34
Get Book Here
Book Description
Author: Robert L. Stallings
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 92
Get Book Here
Book Description
Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack from 0 to 15 degrees.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 714
Get Book Here
Book Description
Author: Clifford Cumming
Publisher: Elsevier
ISBN: 0323141838
Category : Technology & Engineering
Languages : en
Pages : 1006
Get Book Here
Book Description
Progress in Astronautics and Rocketry, Volume 10: Technology of Lunar Exploration is an overview of the technical base of the lunar exploration problem. This volume is organized into six sections encompassing 35 that follow the various stages of accomplishment of a lunar mission, involving landing on or orbiting the moon and returning to the earth. The first section is devoted to the problem of trying to define the lunar environment, emphasizing the theories of the lunar environment as it relates to the internal structure of the moon. This section also describes some activities to achieve a reasonable theory concerning what might be encountered in some of the previous lunar flight programs. The second section explores the problems associated with the limitations imposed upon lunar missions by the launch vehicles and launching facilities. The third section looks at the spacecraft systems and techniques required for lunar missions, particularly the technology and specific subsystems in relation to the requirements imposed by specific lunar mission objectives. The fourth section deals with the actual landing on the moon and the subsequent surface operations, while the fifth section covers the lunar launch, return, flight re-entry, and subsequent landing on earth. The sixth section reports the status of the projects that represent the United States lunar exploration program, which integrates the technologies developed in the preceding sections into certain discrete projects.
Author: Konstantin Volkov
Publisher: BoD – Books on Demand
ISBN: 1789232643
Category : Science
Languages : en
Pages : 372
Get Book Here
Book Description
The book focuses on new analytical, experimental, and computational developments in the field of research of heat and mass transfer phenomena. The generation, conversion, use, and exchange of thermal energy between physical systems are considered. Various mechanisms of heat transfer such as thermal conduction, thermal convection, thermal radiation, and transfer of energy by phase changes are presented. Theory and fundamental research in heat and mass transfer, numerical simulations and algorithms, experimental techniques, and measurements as they applied to all kinds of applied and emerging problems are covered.
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1352
Get Book Here
Book Description
Author: George E. Kaattari
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 28
Get Book Here
Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 190
Get Book Here
Book Description
Author: William R. Wells
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 312
Get Book Here
Book Description
Newtonian closed-form expressions for the aerodynamic coefficients are developed for complete and partial conic and spheric bodies at combined angles of attack and sideslip. Calculations from these expressions are presented in tabulated form for various body shapes. Closed-form expressions for some of the static stability derivatives are also presented. Comparisons of this theory with hypersonic experimental data are made for many of the body shapes.
