Masters Diploma in Aircraft Design

Rve Technologies
In Bangalore

Price on request
You can also call the Study Centre
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Important information

Typology Diploma
Location Bangalore
Duration 1 Day
  • Diploma
  • Bangalore
  • Duration:
    1 Day


Where and when

Starts Location
On request
Room 111535,1st Floor, 39th Cross, 25th Main,4th 'T'block, Jayanagar, 560040, Karnataka, India
See map
Starts On request
Room 111535,1st Floor, 39th Cross, 25th Main,4th 'T'block, Jayanagar, 560040, Karnataka, India
See map

Frequent Asked Questions

· Requirements

Students and professionals/Diploma/B.TECH or Equivalent in Aero/Mechanical/Auto/Civil/structural

Course programme

The theory aspects of the program that are included in it are discussed below:
Aircraft component Designing
Aircraft Structural Designing
Structural Modeling
Computer Implementing
The overview of the 3D-Software is as follows:
Generating Drafting, Part designing & Assembling, Welding-Designs, Rivet-Design, Wire-frames and Surfaces, Designs, Aerospace Sheet Metal, Cores and cavity Designs, D.M.U. kinematics, Free-style and Shapers.
The overview of Ansys is: - Pre-Processing, Solutions, & Post-processing, Applications of Ansys to Stress-Analysis, Nodal Analysis, Flow Analysis, Thermal-Analysis and Higher-level Advanced mesh generating tools.
Applicants and professionals/Diploma/B-TECH or equal in Aero/Mechanical/Auto/Civil/structural are eligible to get enrolled into this program.

The contents of the program are as discussed below:

Aircraft components designing:
• The Aircraft-industry, novel aircraft development, Boeing-Airplanes, Air-bus Airplane
• Main Aircraft component and their tasks
• Unit solution, Balancing of force systems
• Indeterminate structure
• The aircraft designing procedure
• Airfoil designing - 2D Uni-graphics and Ansys
• Wing-design
• Landing gear structures and analyzing
• Landing gear designing by use of Uni-graphics and Ansys
• Wing-structure
• Wing designing by use of Uni-graphics and Ansys
• Tail-analysis
• Fuselage shells analyzing
• Fuselage stress analyzing by use of Ansys
• Thermal analyzing
• Deflection analyzing
• Stiffness analyzing
Aircraft Structured Designs
• Designing Life Criteria - Philosophy
• Material
• Structural-Optimization
Structural Modeling, Computer Implementations, F.E.M.,
• Variations in formulation
• Solutions that are unique and that exist
• Discretions
• Selecting a base
• Minute support of the basis
• Matrix form of the trouble
• General-form of the finite elements methods
• Comparing to the finite variation methods
• Distinct kinds of finite element procedures
• General finite elements procedure
• HP-F.E.M.
• HPK-F.E.M.
• X.F.E.M.
• Spectral Techniques
• Mesh-free techniques
• Dis-continuous Galerkin-methods
• Finite Elements in Limiting Analysis
• Property of section, centroid, moments of inertia for aircrafts
• Basic structural load on air-craft
• V-n diagrams and gust-diagrams
• F.A.R. requirement

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