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...

Full description

Bibliographic Details
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
_version_ 1797368751984738304
author Kyong Chol Chou
author_facet Kyong Chol Chou
author_sort Kyong Chol Chou
collection DOAJ
description 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-state loads, overall steady-state loads, buffet, ground wind loads, base heating and rocket-nozzle hinge moments are examined here specifically.
first_indexed 2024-03-08T17:37:15Z
format Article
id doaj.art-b7227308cbcf4ace914ca3ae8dedbb07
institution Directory Open Access Journal
issn 2093-5587
2093-1409
language English
last_indexed 2024-03-08T17:37:15Z
publishDate 1984-09-01
publisher The Korean Space Science Society
record_format Article
series Journal of Astronomy and Space Sciences
spelling doaj.art-b7227308cbcf4ace914ca3ae8dedbb072024-01-02T11:44:13ZengThe Korean Space Science SocietyJournal of Astronomy and Space Sciences2093-55872093-14091984-09-0111521Aerodynamic Problems of Launch VehiclesKyong Chol Chou0Department of Space Science, Kyung Hee UniversityThe 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-state loads, overall steady-state loads, buffet, ground wind loads, base heating and rocket-nozzle hinge moments are examined here specifically.http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1984/v1n1/OJOOBS_1984_v1n1_5.pdf
spellingShingle Kyong Chol Chou
Aerodynamic Problems of Launch Vehicles
Journal of Astronomy and Space Sciences
title Aerodynamic Problems of Launch Vehicles
title_full Aerodynamic Problems of Launch Vehicles
title_fullStr Aerodynamic Problems of Launch Vehicles
title_full_unstemmed Aerodynamic Problems of Launch Vehicles
title_short Aerodynamic Problems of Launch Vehicles
title_sort aerodynamic problems of launch vehicles
url http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/1984/v1n1/OJOOBS_1984_v1n1_5.pdf
work_keys_str_mv AT kyongcholchou aerodynamicproblemsoflaunchvehicles