TY - JOUR
T1 - Wind tunnel free-flight test for multi-bodies separation
AU - Jiang, Zenghui
AU - Song, Wei
AU - Jia, Quyao
AU - Chen, Nong
N1 - Publisher Copyright:
© 2016, The Editorial Board of ACTA AERODYNAMICA SINICA. All right reserved.
PY - 2016/10/1
Y1 - 2016/10/1
N2 - The technique of wind tunnel free-flight test for multi-bodies separation, a more complicated wind tunnel special test technique, has been developed. With this new technique, the multi-bodies separation process of the aircraft can be simulated more accurately, and the whole separation process can be recorded by the high-speed camera. The technique is introduced in detail, include the principle, characteristic, test model design, similarity criteria, and test apparatus. Based on the different characteristic and application fields, the technique of wind tunnel free-flight test for multi-bodies separation can be classified as stage separation, submunition separating from dispenser and multi-bodies separation with additional constraints. Detailed specification is given for each type. The test images and flight path curves of each separated-body are presented. According to the above presentation, the technique of wind tunnel free-flight test for multi-bodies separation, can be well understand and easily adopted by more researchers engaged in wind tunnel test.
AB - The technique of wind tunnel free-flight test for multi-bodies separation, a more complicated wind tunnel special test technique, has been developed. With this new technique, the multi-bodies separation process of the aircraft can be simulated more accurately, and the whole separation process can be recorded by the high-speed camera. The technique is introduced in detail, include the principle, characteristic, test model design, similarity criteria, and test apparatus. Based on the different characteristic and application fields, the technique of wind tunnel free-flight test for multi-bodies separation can be classified as stage separation, submunition separating from dispenser and multi-bodies separation with additional constraints. Detailed specification is given for each type. The test images and flight path curves of each separated-body are presented. According to the above presentation, the technique of wind tunnel free-flight test for multi-bodies separation, can be well understand and easily adopted by more researchers engaged in wind tunnel test.
KW - Multi-bodies separation
KW - Stage separation
KW - Submunition disperse
KW - Wind tunnel free-flight test
UR - https://www.scopus.com/pages/publications/84992411635
U2 - 10.7638/kqdlxxb-2014.0137
DO - 10.7638/kqdlxxb-2014.0137
M3 - 文章
AN - SCOPUS:84992411635
SN - 0258-1825
VL - 34
SP - 581
EP - 586
JO - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
JF - Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica
IS - 5
ER -