Estimation of stiffness derivative for ogives at constant specific heat ratio γ = 1.666 at hypersonic mach numbers
Specific heat ratios play an essential role in the design of an ogive of an aircraft, which in turn makes it a priority point in estimating the stiffness derivative, keeping in mind the stability of an airplane. One such attempt is made here where the study of stiffness derivative is done for specif...
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主要な著者: | Shabana, Aysha, Shamitha, A, Crasta, Asha, Khan, Sher Afghan |
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フォーマット: | 論文 |
言語: | English |
出版事項: |
Turkbilmat Egitim Hizmetleri
2021
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主題: | |
オンライン・アクセス: | http://irep.iium.edu.my/89687/7/89687_Estimation%20of%20stiffness%20derivative%20for%20ogives%20at%20constant%20specific%20heat%20ratio.pdf http://irep.iium.edu.my/89687/ https://turcomat.org/index.php/turkbilmat/article/view/4163 |
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