Aerospace Instrument-Making Annotation << Back CREATION OF COMPUTATIONAL AND EXPERIMENTAL ANALYSIS OF AIRCRAFT ELEMENTS USING SPECKLE INTERFEROMETRY Tun Min Latt, I.V. Volkov This is proposed to create new means of non-destructive testing based on the use of optical, especially speckle-holographic methods of interferometry and interpretation of speckle-holograms in the computational-experimental analysis of aircraft strength. Key words: calculation and experimental method, speckle-holographic interferometry, stress concentration, non-destructive testing of aircraft structures. DOI: 10.25791/aviakosmos.12.2019.1057 Contacts: - Pp. 41-44.