Impulse Analysis of Airplane Crash Data with Consideration Given to Human Tolerance

[1]  S H Robertson,et al.  FULL-SCALE DYNAMIC CRASH TEST OF A DOUGLAS DC-7 AIRCRAFT , 1965 .

[2]  E. Alfaro-Bou,et al.  Light airplane crash tests at three flight-path angles , 1978 .

[3]  E. Alfaro-Bou,et al.  Light airplane crash tests at three pitch angles , 1979 .

[4]  E Alfaro-Bou,et al.  Light Airplane Crash Tests at Impact Velocities of 13 and 27 m/sec , 1977 .

[5]  E. Alfaro-Bou,et al.  Light airplane crash tests at three roll angles , 1979 .

[6]  Gil Wittlin DEVELOPMENT, EXPERIMENTAL VERIFICATION, AND APPLICATION OF PROGRAM "KRASH" FOR GENERAL AVIATION AIRPLANE STRUCTURAL CRASH DYNAMICS , 1978 .

[7]  R. J. Hayduk,et al.  Crash tests of four identical high-wing single-engine airplanes , 1980 .

[8]  Edwin L. Fasanella,et al.  Determination of crash test pulses and their application to aircraft seat analysis , 1981 .

[9]  I Irving Pinkel,et al.  Seat Design for Crash Worthiness , 1957 .

[10]  Gil Wittlin,et al.  FULL SCALE CRASH TEST EXPERIMENTAL VERIFICATION OF A METHOD OF ANALYSIS FOR GENERAL AVIATION STRUCTURAL CRASHWORTHINESS , 1978 .

[11]  A. Martin Eiband Human Tolerance to Rapidly Applied Accelerations: A Summary of the Literature , 1959 .

[12]  H. D. Carden Correlation and assessment of structural airplane crash data with flight parameters at impact , 1982 .

[13]  Robert J. Hayduk,et al.  NASA/FAA general aviation crash dynamics program - An update , 1979 .

[14]  E. Alfaro-Bou,et al.  Impact dynamics research facility for full-scale aircraft crash testing , 1976 .

[15]  M. S. Williams,et al.  Crash tests of four low-wing twin-engine airplanes with truss-reinforced fuselage structure , 1982 .

[16]  Dugald O. Black,et al.  Accelerations and passenger harness loads measured in full-scale light-airplane crashes , 1953 .

[17]  W. H. Reed,et al.  FULL-SCALE DYNAMIC CRASH TEST OF A LOCKHEED CONSTELLATION MODEL 1649 AIRCRAFT , 1965 .