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Authors
D. Vnuchkov
D. Vnuchkov
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Testing of Detonation Ramjet Model in a Wind Tunnel at Approach Air Stream Mach Number 5.7 and Stagnation Temperature 1500 K (Doklady Akademii nauk)
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Publishing LLC
«
Integration: Education and Science
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ras.jes.su
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Publishing LLC «I-PC»
jes.su
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