Author: Rudolf HermannPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 410
Book Description
Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics
Author: Rudolf HermannPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 410
Book Description
Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics
Author: Rudolf HermannPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 408
Book Description
Supersonic Inlet Diffusers and Introduction to Internal Aerodymanics
Author: Rudolf HermannHandbook of Supersonic Aerodynamics
Author: George RudingerPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 452
Book Description
The Use of Perforated Inlets for Efficient Supersonic Diffusion
Author: John C. EvvardPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 40
Book Description
Investigation of Three Types of Supersonic Diffuser Over a Range of Mach Numbers from 1.75 to 2.74
Author: L. Eugene BaughmanPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
An investigation was conducted in the Lewis 4- by 4-inch variable Mach number tunnel to determine off-design internal performance of three types of supersonic diffuser. Results were obtained at Mach numbers ranging from 1.75 to 2.74 with a normal-shock diffuser, two single-shock spike diffusers designed for Mach numbers 1.75 and 2.40, respectively, and tree convergent-divergent perforated diffusers designed for Mach numbers 1.75, 2.10, and 2.50, respectively. The variation of total-pressure recovery with relative mass flow was determined at various Mach numbers in the range. A thrust coefficient based on these measurements was utilized to facilitate interpretation of the results.
Handbook of Supersonic Aerodynamics
Author: Johns Hopkins University. Applied Physics LaboratoryPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 456
Book Description
Supersonic Inlets
Author: Ione D. V. FaroPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 186
Book Description
The design and operation of supersonic inlets is discussed. The means by which the incoming flow may be decelerated to a subsonic velocity are enumerated and evaluated. This report covers diffusers which employ internal compression, external compression or a combination of the two. Experimentally determined values of the total pressure recovery, the capture-area ratio and the inlet drag are compared with those determined from available theories for all types of diffusers. The discussions which in general refer to axisymmetric configurations usually may be applied with equal validity to two-dimensional diffusers. However, some specific problems of the latter are treated. The effects of boundary layer are considered in some detail as are the problems of oscillating flow. (Author).
Applied Gas Dynamics
Author: Ethirajan RathakrishnanPublisher: John Wiley & Sons
ISBN: 1119500389
Category : Science
Languages : en
Pages : 656
Book Description
A revised edition to applied gas dynamics with exclusive coverage on jets and additional sets of problems and examples The revised and updated second edition of Applied Gas Dynamics offers an authoritative guide to the science of gas dynamics. Written by a noted expert on the topic, the text contains a comprehensive review of the topic; from a definition of the subject, to the three essential processes of this science: the isentropic process, shock and expansion process, and Fanno and Rayleigh flows. In this revised edition, there are additional worked examples that highlight many concepts, including moving shocks, and a section on critical Mach number is included that helps to illuminate the concept. The second edition also contains new exercise problems with the answers added. In addition, the information on ram jets is expanded with helpful worked examples. It explores the entire spectrum of the ram jet theory and includes a set of exercise problems to aid in the understanding of the theory presented. This important text: Includes a wealth of new solved examples that describe the features involved in the design of gas dynamic devices Contains a chapter on jets; this is the first textbook material available on high-speed jets Offers comprehensive and simultaneous coverage of both the theory and application Includes additional information designed to help with an understanding of the material covered Written for graduate students and advanced undergraduates in aerospace engineering and mechanical engineering, Applied Gas Dynamics, Second Edition expands on the original edition to include not only the basic information on the science of gas dynamics but also contains information on high-speed jets.
Dynamic Response of a Supersonic Diffuser to Bypass and Spike Oscillation
Author: David N. BowditchPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38
Book Description