Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 614

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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1102

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Author: Holger Babinsky
Publisher: Cambridge University Press
ISBN: 1139498649
Category : Technology & Engineering
Languages : en
Pages : 481

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Book Description
Shock wave-boundary-layer interaction (SBLI) is a fundamental phenomenon in gas dynamics that is observed in many practical situations, ranging from transonic aircraft wings to hypersonic vehicles and engines. SBLIs have the potential to pose serious problems in a flowfield; hence they often prove to be a critical - or even design limiting - issue for many aerospace applications. This is the first book devoted solely to a comprehensive, state-of-the-art explanation of this phenomenon. It includes a description of the basic fluid mechanics of SBLIs plus contributions from leading international experts who share their insight into their physics and the impact they have in practical flow situations. This book is for practitioners and graduate students in aerodynamics who wish to familiarize themselves with all aspects of SBLI flows. It is a valuable resource for specialists because it compiles experimental, computational and theoretical knowledge in one place.

Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 932

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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).

Author: Donald R. Boldman
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 68

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Book Description
A review of a comprehensive experimental investigation of the heat transfer and boundary layer in 30 deg to 15 deg and 60 deg to 15 deg conical nozzles is presented. The experiments were conducted with air at a stagnation temperature of 539 K (970 R) and throat Reynolds numbers based on a diameter ranging from 6 x 10 to the 5th power to 5 x 10 to the 6th power. Nozzle wall surface finish was varied from a smooth machine finish to a 826 x 10 to the minus 6th power cm (325 x 10 to the minus 6th in.) rms sandblasted finish. Measured heat transfer and wall temperatures are tabulated.

Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 590

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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 314

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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 296

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Author: Witold Nowacki
Publisher:
ISBN:
Category : Structural dynamics
Languages : en
Pages : 402

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Author: Viktor Mikhaĭlovich Sheĭnin
Publisher:
ISBN:
Category : Jet transports
Languages : en
Pages : 312

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Book Description