Development of a computer program for rocket aerodynmic coefficients estimation
A computational method has been developed to realize an efficient and accurate user friendly computational program called RocketCalculator, which integrates carefully assessed methodologies and offer flexibilities of the rocket configurations and velocities up to Mach number 3.0 and angle of attack...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English English |
| Published: |
Faculty of Mechanical Engineering, UTM
2009
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| Subjects: | |
| Online Access: | http://eprints.utm.my/21023/1/MdNizamDahalan2009_DevelopmentOfAComputerProgram.pdf http://eprints.utm.my/21023/2/nizam_Rocket-I-2009_28-43.pdf |