Aerodynamic Problems of Launch Vehicles
The airflow along the surface of a launch vehicle together with vase flow of clustered nozzles cause problems which may affect the stability or efficiency of the entire vehicle. The problem may occur when the vehicle is on the launching pad or even during flight. As for such problems, local steady-s...
Main Author: | Kyong Chol Chou |
---|---|
Format: | Article |
Language: | English |
Published: |
The Korean Space Science Society
1984-09-01
|
Series: | Journal of Astronomy and Space Sciences |
Online Access: | http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1984/v1n1/OJOOBS_1984_v1n1_5.pdf |
Similar Items
-
Unsteady aerodynamic investigation of the propeller-wing interaction for a rocket launched unmanned air vehicle
by: Zhang, G. Q., et al.
Published: (2013) -
Aerodynamic characteristics of a novel catapult launched morphing tandem-wing unmanned aerial vehicle
by: Liang Gao, et al.
Published: (2017-02-01) -
Research of the launch vehicle design made of composite materials under the aerodynamic, thermal and acoustic loadings
by: Davydovich Denis, et al.
Published: (2017-01-01) -
Unsteady Aerodynamic Investigation of the Propeller-Wing Interaction for a Rocket Launched Unmanned Air Vehicle
by: G. Q. Zhang, et al.
Published: (2013-01-01) -
Low-Cost Satellite Launch System—Aerodynamic Feasibility Study
by: Aleksander Olejnik, et al.
Published: (2022-05-01)