Analysis for determining dynamic response of airplanes to runway unevenness during takeoff or landing was programmed for numerical solution on IBM 7090 digital computer; analysis permits inclusion of landing gear nonlinear characteristics and flexural mode characteristics of free-free airframe; dynamic response of Boeing 733-94 supersonic airplane and Boeing 707 airplane on Runway 12, Langley Field, and on Runway 28R, San Francisco International Airport was determined.
Response of supersonic transports to runway unevenness
ASCE -- Proc (J AeroSpace Transport Div)
1966
20 pages
Article (Journal)
English
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NTIS | 1973
Online Contents | 1994
Materials for supersonic transports
AIAA | 1964
|Ramjet-powered supersonic transports
Engineering Index Backfile | 1959
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