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Design and development of aerospace ...

International Symposium on Applied Aerodynamics and Design of Aerospace Vehicles ((2018 :)

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Design and development of aerospace vehicles and propulsion systems = proceedings of SAROD 2018 /

Record Type:	Electronic resources : Monograph/item
Title/Author:	Design and development of aerospace vehicles and propulsion systems/ edited by S. Kishore Kumar, Indira Narayanaswamy, V. Ramesh.
Reminder of title:	proceedings of SAROD 2018 /
remainder title:	SAROD 2018
other author:	Kumar, S. Kishore.
corporate name:	International Symposium on Applied Aerodynamics and Design of Aerospace Vehicles
Published:	Singapore :Springer Singapore : : 2021.,
Description:	x, 532 p. :ill., digital ;24 cm.
[NT 15003449]:	Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due To Chevron -- Parametric Study of Turbulent Flow Past a Compression Decompression Ramp -- Validation of Numerical Analysis Results for Pusher Configured Turboprop Engine Air Intake -- Aero-Elastic Analysis of High Aspect Ratio UAV Wing - Based on Two-Way Fluid Structure Interaction -- Numerical Study of Effect of Adjacent Blades Oscillation in a Compressor Cascade -- Effect of Incoming Wakes on Losses of a Low Pressure Turbine of a Gas Turbine Engine -- Effect of Axial Location on the Performance of A Control Jet In A Supersonic Cross Flow.
Contained By:	Springer Nature eBook
Subject:	Aerodynamics - Congresses. -
Online resource:	https://doi.org/10.1007/978-981-15-9601-8
ISBN:	9789811596018

Design and development of aerospace vehicles and propulsion systems = proceedings of SAROD 2018 /
Design and development of aerospace vehicles and propulsion systemsproceedings of SAROD 2018 /[electronic resource] :SAROD 2018edited by S. Kishore Kumar, Indira Narayanaswamy, V. Ramesh. - Singapore :Springer Singapore :2021. - x, 532 p. :ill., digital ;24 cm. - Lecture notes in mechanical engineering,2195-4356. - Lecture notes in mechanical engineering..

Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due To Chevron -- Parametric Study of Turbulent Flow Past a Compression Decompression Ramp -- Validation of Numerical Analysis Results for Pusher Configured Turboprop Engine Air Intake -- Aero-Elastic Analysis of High Aspect Ratio UAV Wing - Based on Two-Way Fluid Structure Interaction -- Numerical Study of Effect of Adjacent Blades Oscillation in a Compressor Cascade -- Effect of Incoming Wakes on Losses of a Low Pressure Turbine of a Gas Turbine Engine -- Effect of Axial Location on the Performance of A Control Jet In A Supersonic Cross Flow.

This book presents selected papers presented in the Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2018), which was jointly organized by Aeronautical Development Agency (the nodal agency for the design and development of combat aircraft in India), Gas-Turbine Research Establishment (responsible for design and development of gas turbine engines for military applications), and CSIR-National Aerospace Laboratories (involved in major aerospace programs in the country such as SARAS program, LCA, Space Launch Vehicles, Missiles and UAVs) It brings together experiences of aerodynamicists in India as well as abroad in Aerospace Vehicle Design, Gas Turbine Engines, Missiles and related areas. It is a useful volume for researchers, professionals and students interested in diversified areas of aerospace engineering.

ISBN: 9789811596018

Standard No.: 10.1007/978-981-15-9601-8doiSubjects--Topical Terms:

691265
Aerodynamics
--Congresses.

LC Class. No.: TL570

Dewey Class. No.: 629.1323

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520 $a This book presents selected papers presented in the Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2018), which was jointly organized by Aeronautical Development Agency (the nodal agency for the design and development of combat aircraft in India), Gas-Turbine Research Establishment (responsible for design and development of gas turbine engines for military applications), and CSIR-National Aerospace Laboratories (involved in major aerospace programs in the country such as SARAS program, LCA, Space Launch Vehicles, Missiles and UAVs) It brings together experiences of aerodynamicists in India as well as abroad in Aerospace Vehicle Design, Gas Turbine Engines, Missiles and related areas. It is a useful volume for researchers, professionals and students interested in diversified areas of aerospace engineering.
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