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001435208 001__ 1435208
001435208 003__ OCoLC
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001435208 019__ $$a1249944224
001435208 020__ $$a9789811596018$$q(electronic bk.)
001435208 020__ $$a9811596018$$q(electronic bk.)
001435208 020__ $$z9789811596001$$q(print)
001435208 0247_ $$a10.1007/978-981-15-9601-8$$2doi
001435208 035__ $$aSP(OCoLC)1243544572
001435208 040__ $$aEBLCP$$beng$$epn$$cEBLCP$$dGW5XE$$dOCLCO$$dEBLCP$$dOCLCF$$dINU$$dOCLCO$$dLEATE$$dBDX$$dUKAHL$$dN$T$$dOCLCO$$dOCLCQ$$dCOM$$dOCLCO$$dOCLCQ
001435208 049__ $$aISEA
001435208 050_4 $$aTL570
001435208 08204 $$a629.132/3$$223
001435208 1112_ $$aSymposium on Applied Aerodynamics and Design of Aerospace Vehicles$$n(8th :$$d2018 :$$cBangalore, India)
001435208 24510 $$aDesign and development of aerospace vehicles and propulsion systems :$$bproceedings of SAROD 2018 /$$cS. Kishore Kumar, Indira Narayanaswamy, V. Ramesh, editors.
001435208 2463_ $$aSAROD 2018
001435208 260__ $$aSingapore :$$bSpringer,$$c2021.
001435208 300__ $$a1 online resource (529 pages)
001435208 336__ $$atext$$btxt$$2rdacontent
001435208 337__ $$acomputer$$bc$$2rdamedia
001435208 338__ $$aonline resource$$bcr$$2rdacarrier
001435208 4901_ $$aLecture Notes in Mechanical Engineering
001435208 500__ $$a2.3 Mathematical Model.
001435208 5050_ $$aIntro -- Contents -- About the Editors -- Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due to Chevron -- 1 Introduction -- 2 Experimental Setup and Test Nozzle -- 3 Experimental Methods -- 4 Results -- 4.1 Aerodynamics Results -- 4.2 Acoustics Results -- 5 Conclusion -- References -- Parametric Study of Turbulent Flow Past a Compression-Decompression Ramp -- 1 Introduction -- 2 Flowfield in the Vicinity of CDR -- 3 Solver Validation -- 4 Grid Independence -- 5 Simulation Parameters -- 6 Simulation Results -- 6.1 Flow Features -- 6.2 Separated Flow Extents
001435208 5058_ $$a7 Summary -- References -- Validation of Numerical Analysis Results for Pusher Configured Turboprop Engine Air Intake -- 1 Introduction -- 2 Geometry and Analysis -- 2.1 Geometry Details -- 2.2 Mesh Details -- 2.3 Numerical Details -- 2.4 Boundary Conditions -- 3 CFD Results and Validation -- 3.1 Computational Results -- 3.2 Instrumentation and Flight Test -- 3.3 Validation -- 4 Conclusion -- References -- Aero-elastic Analysis of High Aspect Ratio UAV Wing-Based on Two-Way Fluid Structure Interaction -- 1 Introduction -- 2 Aero-elasticity -- 3 Fluid-Structure Interaction
001435208 5058_ $$a3.1 Monolithic Approach -- 3.2 Partitioned Approach -- 3.3 Data Mapping -- 4 Model Generation -- 4.1 Flat Composite Plate Wing Divergence Study -- 4.2 Large AR Wing Divergence Study -- 5 Mesh and Boundary Conditions -- 5.1 Finite Elements Analysis -- 5.2 Computational Fluid Dynamics -- 6 Solver Setup -- 6.1 Computational Fluid Dynamics (CFD) -- 6.2 Finite Element Method (FEM) -- 6.3 System Coupling -- 6.4 Input Parameters -- 7 Results and Discussion -- 7.1 Grid Independence Study -- 8 Validation -- 8.1 Flat Composite Plate Wing Divergence Study -- 8.2 Large AR Wing Divergence Study
001435208 5058_ $$a9 Conclusion -- References -- Numerical Study of Effect of Adjacent Blades Oscillation in a Compressor Cascade -- 1 Introduction -- 2 Numerical Setup -- 3 Results and Discussion -- 3.1 Validation -- 3.2 Effect of Reduced Frequency -- 3.3 Effect of Stagnation Point Location on Reattachment Length -- 4 Conclusions -- References -- Effect of Incoming Wakes on Losses of a Low-Pressure Turbine of a Gas Turbine Engine -- 1 Introduction -- 2 Description of the Problem -- 3 Computational Methodology -- 4 Grid Generation -- 5 Boundary Conditions -- 6 Computational Time and Convergence
001435208 5058_ $$a7 Results and Discussion -- 8 Conclusions -- References -- Effect of Axial Location on the Performance of a Control Jet in a Supersonic Cross Flow -- 1 Introduction -- 2 Methodology -- 3 Validation and Grid Independence Study -- 4 Results -- 4.1 Shock Structures -- 4.2 Vortex Structures -- 4.3 Surface Pressure Distribution -- 4.4 Force and Moment Due to Interaction -- 4.5 Jet Effectiveness -- 5 Conclusion -- References -- Effect of Chord Variation on Subsonic Aerodynamics of Grid Fins -- 1 Introduction -- 2 Numerical Methodology -- 2.1 Geometry -- 2.2 Mesh and Boundary Conditions
001435208 506__ $$aAccess limited to authorized users.
001435208 520__ $$aThis book presents selected papers presented in the Symposium on Applied Aerodynamics and Design of Aerospace Vehicles (SAROD 2018), which was jointly organized by Aeronautical Development Agency (the nodal agency for the design and development of combat aircraft in India), Gas-Turbine Research Establishment (responsible for design and development of gas turbine engines for military applications), and CSIR-National Aerospace Laboratories (involved in major aerospace programs in the country such as SARAS program, LCA, Space Launch Vehicles, Missiles and UAVs). It brings together experiences of aerodynamicists in India as well as abroad in Aerospace Vehicle Design, Gas Turbine Engines, Missiles and related areas. It is a useful volume for researchers, professionals and students interested in diversified areas of aerospace engineering.
001435208 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed April 7, 2021).
001435208 650_0 $$aAerodynamics$$vCongresses.
001435208 650_0 $$aAerospace engineering$$vCongresses.
001435208 650_6 $$aAérodynamique$$vCongrès.
001435208 650_6 $$aAérospatiale (Ingénierie)$$vCongrès.
001435208 655_7 $$aConference papers and proceedings.$$2fast$$0(OCoLC)fst01423772
001435208 655_7 $$aConference papers and proceedings.$$2lcgft
001435208 655_7 $$aActes de congrès.$$2rvmgf
001435208 655_0 $$aElectronic books.
001435208 7001_ $$aKumar, S. Kishore.
001435208 7001_ $$aNarayanaswamy, Indira.
001435208 7001_ $$aRamesh, V.
001435208 77608 $$iPrint version:$$aKumar, S. Kishore.$$tDesign and Development of Aerospace Vehicles and Propulsion Systems.$$dSingapore : Springer Singapore Pte. Limited, ©2021$$z9789811596001
001435208 830_0 $$aLecture notes in mechanical engineering.
001435208 852__ $$bebk
001435208 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-981-15-9601-8$$zOnline Access$$91397441.1
001435208 909CO $$ooai:library.usi.edu:1435208$$pGLOBAL_SET
001435208 980__ $$aBIB
001435208 980__ $$aEBOOK
001435208 982__ $$aEbook
001435208 983__ $$aOnline
001435208 994__ $$a92$$bISE