A description of a special type of seismograph, called a "landing-shock recorder," to be used for measuring the acceleration during impacts such as are experienced in airplane landings, is given . The theory, together with the assumptions made, is discussed in its relation to calculating the acceleration experienced in impact. Calculations are given from records obtained for two impacts of known acceleration. In one case the impact was very severe and in the other it was only moderately severe
Two similar general aviation airplanes were crash tested at the Langley impact dynamics research fac...
An aircraft landing may be described as a controlled crash because a runway surface is intercepted. ...
From a total of 351 instrumentation channels, 341 channels (97%) were in operation during the initia...
A description of a special type of seismograph, called a "landing-shock recorder," to be used for me...
In connection with the development of an accelerometer for measuring the loads on airplanes in free ...
This report deals with the accelerations obtained in flight on various airplanes at Langley Field fo...
A discussion is given of the behavior of the shock-absorbing system, consisting of elastic struts an...
Measurement of perpendicular impacts of a landing gear with different shock-absorbing struts against...
Dynamic response to impact loadings of acceleration sensors having various mounting characteristic
Crash deceleration pulse data from a crash dynamics program on general aviation airplanes and from t...
On December 1, 1984, the FAA and NASA conducted a remotely piloted air-to-ground crash test of a Boe...
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautical Engineering, 1924by ...
Report deals with the impact forces in landing gears. Both the landing impact and the taxiing impact...
It was found that the sampling rates from flight recorders on a remotely piloted transport aircraft ...
1. The Object, of the present Seismograph. It his been too difficult for the hitherto built seismogr...
Two similar general aviation airplanes were crash tested at the Langley impact dynamics research fac...
An aircraft landing may be described as a controlled crash because a runway surface is intercepted. ...
From a total of 351 instrumentation channels, 341 channels (97%) were in operation during the initia...
A description of a special type of seismograph, called a "landing-shock recorder," to be used for me...
In connection with the development of an accelerometer for measuring the loads on airplanes in free ...
This report deals with the accelerations obtained in flight on various airplanes at Langley Field fo...
A discussion is given of the behavior of the shock-absorbing system, consisting of elastic struts an...
Measurement of perpendicular impacts of a landing gear with different shock-absorbing struts against...
Dynamic response to impact loadings of acceleration sensors having various mounting characteristic
Crash deceleration pulse data from a crash dynamics program on general aviation airplanes and from t...
On December 1, 1984, the FAA and NASA conducted a remotely piloted air-to-ground crash test of a Boe...
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautical Engineering, 1924by ...
Report deals with the impact forces in landing gears. Both the landing impact and the taxiing impact...
It was found that the sampling rates from flight recorders on a remotely piloted transport aircraft ...
1. The Object, of the present Seismograph. It his been too difficult for the hitherto built seismogr...
Two similar general aviation airplanes were crash tested at the Langley impact dynamics research fac...
An aircraft landing may be described as a controlled crash because a runway surface is intercepted. ...
From a total of 351 instrumentation channels, 341 channels (97%) were in operation during the initia...