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...
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Format: | Article |
Language: | English |
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The Korean Space Science Society
1984-09-01
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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 |
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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 |