References
- Carden , H. D. 1982 . Correlation and assessment of structural airplane crash data with flight parameters at impact . NASA Technical Paper 2083, National Aeronautics and Space Administration, Hampton, VA
- Coltman , J. W. , Bolukasi , A. O. and Laananen , D. H. 1985 . Analysis of rotorcraft crash dynamics for development of improved crashworthiness design criteria , Atlantic City Airport , NJ : Federal Aviation Administration . DOT/FAA/CT-85/11
- Crash Survival Design Guide . 1971 . USAAMRDL Technical Report 71-22, U.S. Army Air Mobility Research and Development Laboratory, Fort Eustis, VA
- Dobbs , M. W. 2010 . Aircraft accident reconstruction: comparison of data . Int. J. Crashworthiness. , 15 ( 3 ) : 281 – 291 . doi: 10.1080/13588260903335092
- Dobbs , M. W. , Boldrick , M. S. , Ericson , H. R. and Rafter , S. D. 2011 . Documentation of evidence and calculation of acceleration in aircraft accident reconstruction . Int. J. Crashworthiness. , 16 ( 2 ) : 117 – 133 . doi: 10.1080/13588265.2010.526393
- Eiband , A. M. 1959 . Human tolerance to rapidly applied accelerations: A summary of the literature , Cleveland , OH : National Aeronautics and Space Administration . NASA Memorandum 5-19-59E
- Hooper , S. J. and Ellis , D. R. 1997 . Aviation safety and crashworthy seat design . Int. J. Crashworthiness. , 2 ( 1 ) : 39 – 53 . doi: 10.1533/cras.1997.0034
- Huculak , R. D. and Lankarani , H. M. 2013 . Use of Euler parameters for the evaluation of ATD head trajectory from angular rate sensor and accelerometer data in aircraft seat certification testing . Int. J. Crashworthiness. , 18 ( 2 ) : 174 – 182 . doi: 10.1080/13588265.2013.766404
- Jackson , K. E. , Boitnott , R. L. , Fasanella , E. L. , Jones , L. E. and Lyle , K. H. 2004 . A history of full-scale aircraft and rotorcraft crash testing and simulation at NASA Langley Research Center , Lisbon , Portugal : Fourth Triennial International Aircraft and Cabin Safety Research Conference .
- King , A. I. 1985 . Regional tolerance to impact acceleration, in Crash Dynamics of General Aviation Aircraft , 29 – 38 . Warrendale , PA : Society of Automotive Engineers . SP-622
- Laananen , D. H. and Winkelman , K. L. 1996 . Analysis of energy-absorbing seat configurations for aircraft . Int. J. Crashworthiness. , 1 ( 4 ) : 355 – 367 . doi: 10.1533/cras.1996.0026
- National Transportation Safety Board . 1983 . General aviation crashworthiness project, phase I , Washington , DC : National Transportation Safety Board . NTSB/SR-83/01
- National Transportation Safety Board . 1985 . General aviation crashworthiness project, phase II – Impact severity and potential injury prevention in general aviation accidents , Washington , DC : National Transportation Safety Board . NTSB/SR-85/01
- National Transportation Safety Board . 1985 . General aviation crashworthiness project, phase III – Acceleration loads and velocity changes of survivable general aviation accidents , Washington , DC : National Transportation Safety Board . NTSB/SR-85/02
- Society of Automotive Engineers . 2005 . “ Performance standards for seats in civil rotorcraft, transport aircraft, and general aviation aircraft ” . In Aerospace Standard AS8049 Rev. B , Warrendale , PA : Society of Automotive Engineers .
- Snyder , R. G. 1973 . “ Impact ” . In Bioastronautics Data Book, 2nd ed. , Edited by: Parker , J. F. Jr. and West , V. R. 221 – 305 . Washington , DC : National Aeronautics and Space Administration . NASA SP-3006
- Soltis , S. J. and Olcott , J. W. 1985 . “ The development of dynamic performance standards for general aviation aircraft seats ” . In Crash Dynamics of General Aviation Aircraft , 39 – 54 . Warrendale , , PA : Society of Automotive Engineers . SP-622
- Swearingen , J. J. 1971 . General aviation structures directly responsible for trauma in crash decelerations , Washington , DC : Federal Aviation Administration . FAA-AM-71-3