METHODS FOR THE STUDY OF FLIGHT LOADS OF AIRCRAFT
Background. As is known, the rocket must have sufficient strength and withstand all loads during operation. The test of the design of the rocket for strength can be carried out in two ways: on workloads or by calculated loads exceeding workers. When studying the loads acting on the rocket, special...
Enregistré dans:
| Auteurs principaux: | , , , |
|---|---|
| Format: | article |
| Langue: | EN RU |
| Publié: |
Penza State University Publishing House
2021
|
| Sujets: | |
| Accès en ligne: | https://doaj.org/article/0473c243e5384bc59b18fc15a2719cde |
| Tags: |
Ajouter un tag
Pas de tags, Soyez le premier à ajouter un tag!
|