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Fluidmechanik
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The Flying Man : Otto Lilienthal – Geschichte, Flüge und Fotografien
Supersonic wake-jet interaction on a rocket afterbody with dual-bell nozzles
Adaptive compensation of nonlinear actuators for flight control applications
CFD Analysis on Aerodynamic Drag Reduction of Pickup Vehicles Using Rear Spoiler
Effect of Tyre Inflation Pressure on Fuel Consumption and Vehicle Handling Performance
Analysis of Propeller by Panel Method for Transport Aircraft
Robust Flutter Prediction of an Airfoil Including Uncertainties
3D Computational Studies of Flapping Wing in Frontal Gusty Shear Flow
Effect of Incoming Wakes on Losses of a Low-Pressure Turbine of a Gas Turbine Engine
Effect of Reynolds Number on Typical Civil Transport Aircraft
Aerodynamic Optimization of Transonic Wing for Light Jet Aircraft
Numerical Study of Effect of Adjacent Blades Oscillation in a Compressor Cascade
Validation of Numerical Analysis Results for Pusher Configured Turboprop Engine Air Intake
Multi-objective Optimization Approach for Low RCS Aerodynamic Design of Aerospace Structures
The Effect of Variable Inlet Guide Vanes on the Performance of Military Engine Fan
Shockwave Oscillations Over the Conical Heat Shield Region of a Typical Launch Vehicle at Mach 0.95
Passive Reduction of Aerodynamic Rolling Moment for a Launch Vehicle
Sensitivity of Altitude Variation on Aerodynamics of a Typical Launch Vehicle During Hot Separation
Diverterless Supersonic Intake for a Generic Stealth Fighter Aircraft
Design and Development of Miniature Mass Flow Control Unit for Air-Intake Characterization
Hinge Moment Characterization of All Movable Control Surface
Non-adiabatic Wall Effects on Transonic Shock/Boundary Layer Interaction
An Adjoint Approach for Accurate Shape Sensitivities in 3D Compressible Flows
Effect of Axial Location on the Performance of a Control Jet in a Supersonic Cross Flow
Aero-elastic Analysis of High Aspect Ratio UAV Wing—Based on Two-Way Fluid Structure Interaction
Parametric Study of Turbulent Flow Past a Compression–Decompression Ramp
Design and development of aerospace vehicles and propulsion systems : Proceedings of SAROD 2018
Rotor Flow Analysis in the Presence of Fuselage Using Unsteady Panel Method
Observation of Low-Frequency Shock Oscillation Over a Forward-Facing Step
Mach Number Effect on Aeroacoustic Characteristics of Compressible Jet Due to Chevron