Performance of two load-limiting subfloor concepts in full-scale general aviation airplane crash tests
General Aviation Technology Conference ; 1984 ; Hampton , VA , U.S.A.
01.01.1984
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
General Aviation , Fuselages , Yaw , Dynamic Response , Pilot , Accelerometer , Aeroplane
Aircraft Subfloor Response to Crash Loadings
SAE Technical Papers | 1981
|Crash-Energy-Absorbing Composite Subfloor Structure
NTRS | 1988
|