Showing posts with label aero 2012 projects. Show all posts
Showing posts with label aero 2012 projects. Show all posts

Wednesday, June 19, 2013

CATIA V5 Complete Materials download

3 Axis surface machining
3D functional tolerancing and annotation
Advanced Machining
Advanced meshing tools
Aerospace Sheetmetal Design
Assembly Design
Automotive body in white fastening
Business Process Knowledge Template
CAST AND FORGED part optimiser
CATIA CADCAM Interface
CATIA Infrastructure Installation Guide
CATIA infrastructure User guide
CATIA INSTANT COLLABORATIVE DESIGN
Circuit Board
Compartment access
Component Catalogue Editor
Composites Design
Core and Cavity Design
Data exchange interfaces
DefaultAUX2V4ToV5withGVS
DefaultAUX2V4ToV5withOptions
Digitised Shape editor
DMU Engineering Analysis Review
DMU fitting simulator
DMU Kinematics Simulator
DMU Navigator
DMU optimiser
DMU Space analysis
DMU space engineering assistant installation guide
DMU space engineering assistant user guide
Electrical 3D design and documentation
Electrical Cableway routing
Electrical connectivity diagram
Electrical harness flattening
Electrical harness instalation
Electrical library
Electrical Systems functional definition
Electrical wire routing
Elffini solver verification
Enovia catia interoperability
Equipment Arrangement
Equipment support structure
Fastening review
Finite Elements reference guide
Free style shape optimiser and profiler
Free style sketch tracer
Functional Moulded Part
Generative Drafting

Thursday, March 1, 2012

CANARD PLANE PROJECT


Aim :- To build a RC(Remote Controlled) Canard
Plane.
What is canard plane? 
Canard is an airframe configuration of fixed wing aircraft in which the forward surface is smaller than the rearward, the former being known as the "canard", while the latter is the main wing. In contrast a conventional aircraft has a small horizontal stabilizer behind the main wing.
Canard designs fall into two main classes:-
a) Lifting canard:- In this configuration, the weight of the aircraft is shared between the main wing and the canard wing
b) Control canard:- most of the weight of the aircraft is carried by the main wing and the canard wing is used primarily for longitudinal control during maneuvering. The pros and cons of the canard versus conventional configurations are numerous and complex, and it is impossible to say which is superior without considering a specific design application.

Various Parameters involved in the design of Canard Plane:-