Estimation of energetic efficiency of heat supply in front of the aircraft at supersonic accelerated flight. Part II. Mathematical model of the trajectory boost part and computational results

✍ Scribed by A. F. Latypov

• Book ID: 107382267
• Publisher: International Academic Publishing Co (Nauka/Interperiodica)
• Year: 2009
• Tongue: English
• Weight: 275 KB
• Volume: 16
• Category: Article
• ISSN: 0869-8643
• DOI: 10.1007/s11510-009-0001-2