Analysis and trends of main parameters (such as takeoff and landing mass, wing specific loading, thrust-toweight ratio and takeoff and landing performance) variation of transport category airplane modifications is given. It is established, that main distinguisher of modification is its too much flight productivity in terms of “payloadrange”, which just leads to variation of the main parameters mentioned above. It is obvious, that takeoff mass increases by 10...20…20 % of fuselage length up to 20 %, required airfield length up to 20…30 % It is stressed, that problem to keep takeoff and landing performance of modification with increased mass and wing specific loading is still actual scientific and practical task.
TRENDS IN CHANGING THE MAIN PARAMETERS WHEN CREATING MODIFICATIONS TO THE TRANSPORT CATEGORY AIRCRAFT
2017
Article (Journal)
Electronic Resource
Unknown
Metadata by DOAJ is licensed under CC BY-SA 1.0
Civil Certification of Avionics Modifications in Military Transport Category Aircraft
SAE Technical Papers | 1997
|Civil Certification of Avionics Modifications in Military Transport Category Aircraft
British Library Conference Proceedings | 1997
|ECONOMIC NEED CREATING MODIFICATIONS OF DOMESTIC MILITARY TRANSPORT AIRCRAFT
DOAJ | 2019
Transport category aircraft systems
SLUB | 1990
|