Control of vibrational power input to semi-infinite anisotropic beam
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 |
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Faculty of Mechanical Engineering
2009
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| Subjects: | |
| Online Access: | http://eprints.utm.my/7948/1/MdNizamDahalan2009_DevelopmentOfAComputerProgram.pdf |
| _version_ | 1825910124787531776 |
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| author | Dahalan, Md. Nizam Su, Vin Cent Ammoo, Mohd. Shariff |
| author_facet | Dahalan, Md. Nizam Su, Vin Cent Ammoo, Mohd. Shariff |
| author_sort | Dahalan, Md. Nizam |
| collection | ePrints |
| description | 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 of 25 degrees. The RocketCalculator is capable of analyzing the configurations of wing-alone, bodyalone, wing-body combination, and wing-body-tail combination of rocket. USAF Datcom Method has been chosen as the analysis method and the programming language is Microsoft Visual Basic. The result would be displayed in form of the corresponding lift (CL ), normal force (CN ) and drag (CD ) coefficients at certain Mach number and angle of attack. Experimented data for several models have been taken out from available sources to validate the program output. Comparisons of the program output and experimental results generally show good agreement with average error of less than 10% |
| first_indexed | 2024-03-05T18:12:22Z |
| format | Article |
| id | utm.eprints-7948 |
| institution | Universiti Teknologi Malaysia - ePrints |
| language | English |
| last_indexed | 2024-03-05T18:12:22Z |
| publishDate | 2009 |
| publisher | Faculty of Mechanical Engineering |
| record_format | dspace |
| spelling | utm.eprints-79482010-09-21T03:31:57Z http://eprints.utm.my/7948/ Control of vibrational power input to semi-infinite anisotropic beam Dahalan, Md. Nizam Su, Vin Cent Ammoo, Mohd. Shariff TJ Mechanical engineering and machinery 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 of 25 degrees. The RocketCalculator is capable of analyzing the configurations of wing-alone, bodyalone, wing-body combination, and wing-body-tail combination of rocket. USAF Datcom Method has been chosen as the analysis method and the programming language is Microsoft Visual Basic. The result would be displayed in form of the corresponding lift (CL ), normal force (CN ) and drag (CD ) coefficients at certain Mach number and angle of attack. Experimented data for several models have been taken out from available sources to validate the program output. Comparisons of the program output and experimental results generally show good agreement with average error of less than 10% Faculty of Mechanical Engineering 2009-06 Article PeerReviewed application/pdf en http://eprints.utm.my/7948/1/MdNizamDahalan2009_DevelopmentOfAComputerProgram.pdf Dahalan, Md. Nizam and Su, Vin Cent and Ammoo, Mohd. Shariff (2009) Control of vibrational power input to semi-infinite anisotropic beam. Jurnal Mekanikal (28). pp. 28-43. ISSN 0127-3396 http://jurnalmekanikal.fkm.utm.my/UserFiles/file/nizam_Rocket-I-2009_28-43.pdf |
| spellingShingle | TJ Mechanical engineering and machinery Dahalan, Md. Nizam Su, Vin Cent Ammoo, Mohd. Shariff Control of vibrational power input to semi-infinite anisotropic beam |
| title | Control of vibrational power input to semi-infinite anisotropic beam |
| title_full | Control of vibrational power input to semi-infinite anisotropic beam |
| title_fullStr | Control of vibrational power input to semi-infinite anisotropic beam |
| title_full_unstemmed | Control of vibrational power input to semi-infinite anisotropic beam |
| title_short | Control of vibrational power input to semi-infinite anisotropic beam |
| title_sort | control of vibrational power input to semi infinite anisotropic beam |
| topic | TJ Mechanical engineering and machinery |
| url | http://eprints.utm.my/7948/1/MdNizamDahalan2009_DevelopmentOfAComputerProgram.pdf |
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