Author: Alastair Cooke
Publisher: John Wiley & Sons
ISBN: 1405172541
Category : Technology & Engineering
Languages : en
Pages : 384
Get Book Here
Book Description
Although a number of texts on helicopter aerodynamics have been written, few have explained how the various theories concerning rotorborne flight underpin practical flight test and evaluation. This book combines theoretical information on aerodynamics, stability, control and performance with details of evaluation methodologies and practical guidance on the conduct of helicopter flight tests. For each topic the relevant theory is explained briefly and followed by details of the practical aspects of testing a conventional helicopter. These include: * safety considerations * planning the tests * the most efficient way to conduct individual flights Where possible typical test results are presented and discussed. The book draws on the authors' extensive experience in flight test and flight test training and will appeal not only to professionals working in the area of rotorcraft test and evaluation, but also to helicopter pilots, rotorcraft designers and manufacturers and final year undergraduates of aeronautical engineering
![Category III, System Operational Test and Evaluation of UH-1F [helicopter] PDF](https://books.google.com/books/content/images/frontcover/r7BDnQAACAAJ?fife=w80-h100)
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 105
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 31
Get Book Here
Book Description
Modern helicopters usually incorporate many engineering systems (including pilot aiding systems such as autostabilisers and flight directors) which are essential to the safe and effective use of the helicopter. Where the helicopter can be endangered by failure of a system (or of one of its units), that system is termed flight safety critical. In general, the use of those systems should not incur a higher probability of hazard to the helicopter than that considered acceptable from considerations of structural or mechanical failure. In assessing the suitability of a helicopter for its intended mission(s), it has become increasingly important to consider the effects of the various systems provided. In particular, assessments of the implications of systems performance and failures derived from calculation and ground tests should be validated by flight tests. This paper seeks to establish the general principles applicable to the testing in flight of any flight safety critical system, with emphasis on certification rather than system development. It does not deal with the testing of particular systems, but it is hoped that readers will find the principles described readily applicable to specific cases.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Get Book Here
Book Description
Author: United States. Flight Standards Service
Publisher:
ISBN:
Category : Flight training
Languages : en
Pages : 36
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Get Book Here
Book Description
Author: United States. Adjutant-General's Office. Personnel Research Branch
Publisher:
ISBN:
Category : Helicopter pilots
Languages : en
Pages : 28
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 12
Get Book Here
Book Description
Author: United States. Adjutant-General's Office. Personnel Research Branch
Publisher:
ISBN:
Category : Helicopter pilots
Languages : en
Pages : 48
Get Book Here
Book Description
Author: United States. Adjutant-General's Office. Personnel Research Branch
Publisher:
ISBN:
Category : Helicopter pilots
Languages : en
Pages : 52
Get Book Here
Book Description
