TY - GEN
T1 - Research on the jet influence on the mechanical launcher of various ignition height
AU - He, Weidong
AU - Jiang, Yi
AU - Ma, Yanli
PY - 2012
Y1 - 2012
N2 - In order to research the different ignition height of the gas jet on the mechanical ejection launcher, the finite volume method was used, a fully structured grid was used to solve the three-dimensional N-S equations, the quasi-steady in the ignition on the nozzle height of 15m, 30m, 35m and 40m conditions were calculated to obtain the different ignition height under deck hatch, as well as temperature and pressure load distribution launchers. The result provides a mechanical reference for the launcher firing height.
AB - In order to research the different ignition height of the gas jet on the mechanical ejection launcher, the finite volume method was used, a fully structured grid was used to solve the three-dimensional N-S equations, the quasi-steady in the ignition on the nozzle height of 15m, 30m, 35m and 40m conditions were calculated to obtain the different ignition height under deck hatch, as well as temperature and pressure load distribution launchers. The result provides a mechanical reference for the launcher firing height.
KW - ignition height
KW - launching mechanical equipment
KW - numerical simulation
KW - rocket plume
UR - http://www.scopus.com/inward/record.url?scp=84867052402&partnerID=8YFLogxK
U2 - 10.1007/978-3-642-31507-7_11
DO - 10.1007/978-3-642-31507-7_11
M3 - Conference contribution
AN - SCOPUS:84867052402
SN - 9783642315060
T3 - Lecture Notes in Electrical Engineering
SP - 57
EP - 63
BT - Advances in Mechanical and Electronic Engineering
T2 - 2012 International Conference on Mechanical and Electronic Engineering, ICMEE 2012
Y2 - 23 June 2012 through 24 June 2012
ER -