Study made of rocking on curved fuselage under surface, following impact of tail or nose, to convert vertical energy in landing into energy of pitching oscillation in which wing lift changes and aerodynamic damping are important; computations of load and motions for given shapes and load applications for selected aircraft; analysis and experiment indicate that loads and moments are acceptable.
Skid landings of airplanes on rocker-type fuselages
NASA -- Tech Note
1961
61 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Skid landings of airplanes on rocker-type fuselages
TIBKAT | 1961
|Skid Landings of Airplanes on Rocker-Type Fuselages
NTRS | 1961
|Multi-engine airplanes and forced landings
Engineering Index Backfile | 1926
|