عنوان
پدید آورنده
موضوع
رده
QC168.85.S45
QC168
.
85
.
S45
کتابخانه
محل استقرار
INTERNATIONAL STANDARD BOOK NUMBER
(Number (ISBN
3030103293
(Number (ISBN
3319731807
(Number (ISBN
3319731815
(Number (ISBN
9783030103293
(Number (ISBN
9783319731803
(Number (ISBN
9783319731810
Erroneous ISBN
3319731793
Erroneous ISBN
9783319731797
TITLE AND STATEMENT OF RESPONSIBILITY
Title Proper
Shock wave interactions :
General Material Designation
[Book]
Other Title Information
selected articles from the 22nd International Shock Interaction Symposium, University of Glasgow, United Kingdom, 4-8 July 2016 /
First Statement of Responsibility
Konstantinos Kontis, editor.
.PUBLICATION, DISTRIBUTION, ETC
Place of Publication, Distribution, etc.
Cham, Switzerland :
Name of Publisher, Distributor, etc.
Springer,
Date of Publication, Distribution, etc.
[2018]
Date of Publication, Distribution, etc.
©2018
PHYSICAL DESCRIPTION
Specific Material Designation and Extent of Item
1 online resource :
Other Physical Details
illustrations
INTERNAL BIBLIOGRAPHIES/INDEXES NOTE
Text of Note
Includes bibliographical references.
CONTENTS NOTE
Text of Note
Intro; Preface; Committee; International Advisory Committee; Scientific Review Committee; Local Organising Committee; Contents; 1 Scale Effects on the Transition of Reflected Shock Waves; Abstract; 1 Introduction; 2 Experiment; 2.1 40 mm × 80 mm Shock Tube; 2.2 100 mm × 180 mm Shock Tube; 2.3 Flow Visualization and Holographic Interferometry; 3 Numerical Simulation; 4 Results and Discussions; 4.1 Interferometric Observation Over Curved Walls in a 40 mm × 80 mm Shock Tube; 4.2 Streak Recording, Measurement of \theta_{crit}; 4.3 Roughened Wedges.
Text of Note
2.3 Differential ("First-Order") Conditions at the Curved Shock in Nonuniform Flow2.4 Special Shock Strengths. Crocco Point and Constant Pressure (Thomas) Point; 2.5 Application of the Differential Conditions at the Curved Shock in Nonuniform Stream to Jet Flow Analysis; 3 Results and Discussion; 3.1 Flow Vorticity Rate (Stagnation Pressure Gradient) in the Vicinity of the Nozzle Lip; 3.1.1 Plane Jet; 3.1.2 Axisymmetric Jet; 3.2 Incident Shock Strength Variation; 3.2.1 Plane Jet; 3.2.2 Axisymmetric Jet; 3.3 Static Pressure Variation in the Compressed Layer; 3.3.1 Plane Jet.
Text of Note
3.3.2 Axisymmetric Jet4 Conclusion; References; Shock Wave Interaction with a Solid Body Floating in the Air; 1 Introduction; 2 Experimental Apparatus and Method; 2.1 Shock Tube and Optical System; 2.2 Solid-Body Injecting System; 2.3 Image Analysis; 3 Results and Discussion; 3.1 Tuning of Operating Conditions; 3.2 Shadowgraph Images; 3.3 Results from Image Analysis; 4 Conclusions; References; 6 Equation of State of Pure Water, Aqueous Solutions of Sodium Chloride, Gelatin Gel, and Glucose Syrup; 1 Introduction; 2 Experimental Method; 3 Result and Discussion; 3.1 Shock Wave Velocities.
Text of Note
4.4 Results of a 40 mm × 80 mm Shock Tube Experiments4.5 Streak Display of Numerical Simulation; 4.6 Delayed Transition Over Wedges in a 100 mm × 180 mm Shock Tube; 4.7 Delayed Transition of Convex and Concave Walls in a 100 mm × 180 mm Shock Tube; 4.8 Delayed Transition Over Cones in a 100 mm × 180 mm Shock Tube; 4.9 Double Wedges; 4.10 Shock Wave Focusing; 5 Concluding Remarks; References; 2 Transition Effect on Shock Wave Boundary Layer Interaction on Compressor Blade; Abstract; 1 Introduction; 2 Experimental Setup; 3 Results and Discussion; 4 Summary and Conclusions; Acknowledgements.
0
8
8
8
SUMMARY OR ABSTRACT
Text of Note
This edited monograph contains the proceedings of the International Shock Interaction Symposium, which emerged as an heir to both the Mach Reflection and Shock Vortex Interaction Symposia. These scientific biannual meetings provide an ideal platform to expose new developments and discuss recent challenges in the field of shock wave interaction phenomena. The goal of the symposia is to offer a forum for international interaction between young and established scientists in the field of shock and blast wave interaction phenomena. The target audience of this book comprises primarily researchers and experts in the field of shock waves, but the book may also be beneficial for young scientists and graduate students alike.
ACQUISITION INFORMATION NOTE
Source for Acquisition/Subscription Address
Springer Nature
Stock Number
com.springer.onix.9783319731803
OTHER EDITION IN ANOTHER MEDIUM
International Standard Book Number
9783319731797
TOPICAL NAME USED AS SUBJECT
Shock (Mechanics), Congresses.
Shock waves, Congresses.
Fluid mechanics.
Mechanics of fluids.
SCIENCE-- Mechanics-- General.
SCIENCE-- Mechanics-- Solids.
Shock (Mechanics)
Shock waves.
(SUBJECT CATEGORY (Provisional
SCI-- 041000
SCI-- 096000
TGMF
TGMF
TGMF1
DEWEY DECIMAL CLASSIFICATION
Number
531
.
1133
Edition
23
LIBRARY OF CONGRESS CLASSIFICATION
Class number
QC168
.
85
.
S45
PERSONAL NAME - ALTERNATIVE RESPONSIBILITY
Kontis, Konstantinos
CORPORATE BODY NAME - PRIMARY RESPONSIBILITY
International Shock Interaction Symposium(21nd :2016 :, Glasgow, Scotland)
ORIGINATING SOURCE
Date of Transaction
20200823104047.0
Cataloguing Rules (Descriptive Conventions))
pn
ELECTRONIC LOCATION AND ACCESS
Electronic name
مطالعه متن کتاب [Book]
Y
