Computational Fluid Dynamics in Aerospace Engineering
Recent Advances
Published on 31. March 2022
168 pages
978-1-80382-992-0 (ISBN)
Description
Computational fluid dynamics has become the key tool in the aviation industry to enhance the advanced concepts. Aviation industry is the first industry to use simulation tools heavily. Typically, the CFD were used to design the futuristics design and other novel design concepts. In general, the design of aircraft, launch vehicles, missiles and UAV were immensely dependent on the CFD tools for their accurate prediction of various parameters without expensive test facility. In general, CFD used to predict the aerodynamic forces, structural loads, thermal loads, combustion., etc. Implementing the proper tools to the CFD simulations massively reduced the involvement of the experimental testing.
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Content
- Cover1
- Guest editorial: Computational fluiddynamics in aerospace engineering: recentadvances
- Power performance enhancement of vertical axis wind turbines by a novel gurney flap design
- Global adaptive neural backstepping control of a flexible hypersonic vehicle with disturbance estimation
- A simulation of the thermal environment of a plastic body of a new type of launch vehicle at the atmospheric phase of the trajectory
- Parametric and V&V study in a fundamental CFD process: revisiting the lid-driven cavity flow
- Estimation of the virtual masses of a large unconventional airship based on purely analytical method to aid in the preliminary design
- Design, modeling and simulation of a control surface-less tri-tilt-rotor UAV
- Numerical modeling on dynamics of droplet in aircraft wing structure at different velocities
- Development of cost-effective shock tube based on experimental and numerical analysis
- Rotating flow thorough parallel plates with the various inclined magnetic field under the influence of hall current
- Experimental and numerical simulation of the piston engine fueled with alternative fuel blends: CFD approach
- Assessment of flight dynamic and static aeroelastic behaviors for jet transport aircraft subjected to instantaneous high g-loads
- Numerical investigation of heat transfer effectson combusti on in a generic gas turbine burner
- Weight minimization of fiber laminated composite beam for aircraft wing construction using exhaustive enumeration algorithm and numerical modeling
- Investigation of mixing characteristics of coflow rectangular nozzle of aspect ratio 2 and 3
- Analytical modeling on the coloring of certain graphs for applications of air traffic and air scheduling management
- Irregular deviation of flight control surface monitoring for jet transport aircraft
