Abstract

The scaled model flight test is one of the three major technical paths of aerodynamic research, which can be used to study and verify the aerodynamic characteristics, danger boundary, new layout, and new technology of the prototype, with the advantages of short cycle, lower risk, and lower cost. Due to different experimental research purposes, there are different design ideas and schemes for scaled models. With the technological development of power systems such as microturbine engines and electric ducted fans, the scaled model has experienced the stages of non-powered drop flight, rocket-assisted flight, and power-driven free flight. In this paper, two scaled verification models are introduced, the similarity criteria of the scaled model are analyzed, the selection of micro engine is carried out, the ground test methods such as fuel consumption test and moment of inertia test are summarized, some test subjects and results are presented, and the key technologies of the flight test of the scaled model are summarized. The flight test results show that the test method can accurately reflect the aerodynamic characteristics and flight performance of the prototype.

Details

Title
Research on key technologies of scaled model flight testing
Author
Kong, Chuihuan 1 ; Pan, Lijun 1 ; Wu, Dawei 1 ; Ma, Rubing 1 ; Cheng, Changfu 1 ; Yunwen Lou 1 

 Shanghai Aircraft Design and Research Institute, Commercial Aircraft Corporation of China Ltd. , Shanghai , China 
First page
012047
Publication year
2023
Publication date
Dec 2023
Publisher
IOP Publishing
ISSN
17426588
e-ISSN
17426596
Source type
Scholarly Journal
Language of publication
English
ProQuest document ID
2903617468
Copyright
Published under licence by IOP Publishing Ltd. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.