97,10 €
107,89 €
-10% with code: EXTRA
Radio Controlled Aircraft
Radio Controlled Aircraft
97,10
107,89 €
  • We will send in 10–14 business days.
The goal of the book is to guide through the designing, manufacturing and testing of an electrically powered Radio Controlled (RC) aircraft. The design of aircraft is optimized for internal payload system. A systematic process from conceptual design to fabrication and testing is thoroughly followed and explained. Aircraft configuration selection process is done by following a qualitative arguments approach including mission performance, payload storage, stability & control and fabrication. The…
  • SAVE -10% with code: EXTRA

Radio Controlled Aircraft (e-book) (used book) | bookbook.eu

Reviews

Description

The goal of the book is to guide through the designing, manufacturing and testing of an electrically powered Radio Controlled (RC) aircraft. The design of aircraft is optimized for internal payload system. A systematic process from conceptual design to fabrication and testing is thoroughly followed and explained. Aircraft configuration selection process is done by following a qualitative arguments approach including mission performance, payload storage, stability & control and fabrication. The designing and optimization has been carried out using AutoCAD, ANSYS and CFX software. The four implementation stages are followed to bring the design from concept to reality.

EXTRA 10 % discount with code: EXTRA

97,10
107,89 €
We will send in 10–14 business days.

The promotion ends in 21d.07:21:12

The discount code is valid when purchasing from 10 €. Discounts do not stack.

Log in and for this item
you will receive 1,08 Book Euros!?
  • Author: Nisar Ahmed Rana
  • Publisher:
  • ISBN-10: 3639511638
  • ISBN-13: 9783639511635
  • Format: 15.2 x 22.9 x 0.4 cm, minkšti viršeliai
  • Language: English English

The goal of the book is to guide through the designing, manufacturing and testing of an electrically powered Radio Controlled (RC) aircraft. The design of aircraft is optimized for internal payload system. A systematic process from conceptual design to fabrication and testing is thoroughly followed and explained. Aircraft configuration selection process is done by following a qualitative arguments approach including mission performance, payload storage, stability & control and fabrication. The designing and optimization has been carried out using AutoCAD, ANSYS and CFX software. The four implementation stages are followed to bring the design from concept to reality.

Reviews

  • No reviews
0 customers have rated this item.
5
0%
4
0%
3
0%
2
0%
1
0%
(will not be displayed)