HEALTH MONITORING OF AIRCRAFT FUSELAGE STRUCTURES USING ULTRASONIC WAVES
25th:; Congress proceedings, International Council of the Aeronautical Sciences ; 2006 ; Hamburg Germany
01.01.2006
4.7.3
Held on CD-ROM.; Shelved in Conference Index
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Structural health monitoring of an adhesively bonded CFRP aircraft fuselage by ultrasonic Lamb Waves
SAGE Publications | 2020
|Crashworthiness of aircraft fuselage structures
AIAA | 1978
|Aircraft fuselage section, aircraft fuselage and aircraft
Europäisches Patentamt | 2023
|