國立虎尾科技大學 |

Design and Development of Aerospace Vehicles and Propulsion Systems = Proceedings of SAROD 2018 /

紀錄類型:	書目-語言資料,印刷品 : Monograph/item
正題名/作者:	Design and Development of Aerospace Vehicles and Propulsion Systems / edited by S. Kishore Kumar, Indira Narayanaswamy, V. Ramesh.
其他題名:	Proceedings of SAROD 2018 /
其他作者:	Ramesh, V.
面頁冊數:	IX, 532 p. 455 illus., 357 illus. in color.online resource. :
Contained By:	Springer Nature eBook
標題:	Engineering Fluid Dynamics. -
電子資源:	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 Systems Proceedings of SAROD 2018 /[electronic resource] :edited by S. Kishore Kumar, Indira Narayanaswamy, V. Ramesh. - 1st ed. 2021. - IX, 532 p. 455 illus., 357 illus. in color.online resource. - Lecture Notes in Mechanical Engineering,2195-4364. - 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:

670525
Engineering Fluid Dynamics.

LC Class. No.: TL787-4050.22

Dewey Class. No.: 629.1

Design and Development of Aerospace Vehicles and Propulsion Systems = Proceedings of SAROD 2018 /
LDR:02998nam a22004335i 4500 001 1048490
003 DE-He213
005 20210813110223.0
007 cr nn 008mamaa
008 220103s2021 si | s |||| 0|eng d
020 $a 9789811596018 $9 978-981-15-9601-8
024 7 $a 10.1007/978-981-15-9601-8 $2 doi
035 $a 978-981-15-9601-8
050 4 $a TL787-4050.22
050 4 $a TC1-1800
072 7 $a TRP $2 bicssc
072 7 $a TEC002000 $2 bisacsh
072 7 $a TRP $2 thema
072 7 $a TTDS $2 thema
082 0 4 $a 629.1 $2 23
245 1 0 $a Design and Development of Aerospace Vehicles and Propulsion Systems $h [electronic resource] : $b Proceedings of SAROD 2018 / $c edited by S. Kishore Kumar, Indira Narayanaswamy, V. Ramesh.
250 $a 1st ed. 2021.
264 1 $a Singapore : $b Springer Singapore : $b Imprint: Springer, $c 2021.
300 $a IX, 532 p. 455 illus., 357 illus. in color. $b online resource.
336 $a text $b txt $2 rdacontent
337 $a computer $b c $2 rdamedia
338 $a online resource $b cr $2 rdacarrier
347 $a text file $b PDF $2 rda
490 1 $a Lecture Notes in Mechanical Engineering, $x 2195-4364
505 0 $a 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.
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.
650 2 4 $a Engineering Fluid Dynamics. $3 670525
650 2 4 $a Fluid- and Aerodynamics. $3 768779
650 1 4 $a Aerospace Technology and Astronautics. $3 683885
650 0 $a Fluid mechanics. $3 555551
650 0 $a Fluids. $3 671110
650 0 $a Astronautics. $3 646219
650 0 $a Aerospace engineering. $3 686400
700 1 $a Ramesh, V. $e editor. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 1352392
700 1 $a Narayanaswamy, Indira. $e editor. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 1317751
700 1 $a Kumar, S. Kishore. $e editor. $4 edt $4 http://id.loc.gov/vocabulary/relators/edt $3 1349631
710 2 $a SpringerLink (Online service) $3 593884
773 0 $t Springer Nature eBook
776 0 8 $i Printed edition: $z 9789811596001
776 0 8 $i Printed edition: $z 9789811596025
776 0 8 $i Printed edition: $z 9789811596032
830 0 $a Lecture Notes in Mechanical Engineering, $x 2195-4356 $3 1253850
856 4 0 $u https://doi.org/10.1007/978-981-15-9601-8
912 $a ZDB-2-ENG
912 $a ZDB-2-SXE
950 $a Engineering (SpringerNature-11647)
950 $a Engineering (R0) (SpringerNature-43712)