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accelerations obtained B-57 main landing Batterson caused by striking Committee for Aeronautics developed during landing diagrs drag loads developed Dreher and Sidney edge light effective lower mass Elfaka light unit F-9^C nose landing feet per second fighter nose landing forward speeds grating horizontal velocity increase in loads L58C28a National Advisory LANDING AND TAXIING landing gear wheel landing impacts landing-gear loads developed Langley landing larger main landing Loads and Stresses loads caused main landing gear mass vertical acceleration maximum vertical load NACA RM L58C28a National Advisory Committee nose landing gear obtain data obtainable from NACA obtained during landings ous types photograph plain concrete raised 5/8 inch RM L58C28a National runway lights runway surface se1nd show the increase shown in figure speeds of 112 strain gages striking the lights TAXIING TESTS TESTS OVER VARIOUS tical tire track to obtain Transient Dynamic types of runway upper mass vertical VARIOUS TYPES vertical and drag