Design and Development of Aerospace Vehicles and Propulsion Systems
portes grátis
Design and Development of Aerospace Vehicles and Propulsion Systems
Proceedings of SAROD 2018
Kumar, S. Kishore; Narayanaswamy, Indira; Ramesh, V.
Springer Verlag, Singapore
03/2022
532
Mole
Inglês
9789811596032
15 a 20 dias
825
Descrição não disponível.
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
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Aerodynamics of Aerospace Vehicles;Conceptual Design of Aircraft;Turbomachinery Flows;Intake Aerodynamics;Rotorcraft Aerodynamics;Missile and Launch Vehicle Aerodynamics;Internal Weapon Bay Simulations;Aeroacoustics;fluid- and aerodynamics
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
Este título pertence ao(s) assunto(s) indicados(s). Para ver outros títulos clique no assunto desejado.
