PREDICTION OF IN-FLIGHT FUNDAMENTAL MODE OF LAUNCH VEHICLE STRUCTURE FROM TWO POINT GROUND VIBRATION TESTS

✍ Scribed by A. Joshi

• Publisher: Elsevier Science
• Year: 1997
• Tongue: English
• Weight: 151 KB
• Volume: 204
• Category: Article
• ISSN: 0022-460X
• DOI: 10.1006/jsvi.1997.0932