Investigation of a 1/4-scale model of the Republic F-105 airplane in the Langley 19-foot pressure tunnel. Lateral control and directional stability and control characteristics of model equipped with drooped, supersonic-type, elliptical wing-root inlet [PDF]
, 1955 Canoro, P. A., Kelly, H. N.
core +1 more source
Selected annotated instance segmentation sub-volumes from a large scale CT data-set of a historic aircraft. [PDF]
Sci DataGruber R +7 more
europepmc +1 more source
Bombs Away: the First Mission on a Coastal Command Liberator [PDF]
, 2012 Matthews, D. Joseph
core +1 more source
Related searches:
Characterization of Boeing 777 Nose Landing Gear to Better Withstand Rough Landing
International Journal of Engineering Research in Africa, 2023An important role a landing gear plays is that it aids in the landing and takeoff of aircraft. The landing gear must be designed in such a way that it can take these stresses in static and dynamic situations. This is to accommodate both rough and smooth landings that result from various loads acting upon it, such as drag force, vertical load, and side ...
Abdulbaqi Jinadu +3 more
openaire +2 more sources
Vibration Analysis of Nose Landing Gear for A Propeller Aircraft
Aeronautical and Aerospace EngineeringThe main problem in the landing gear dynamics of the aircraft is either shimmy or brake induced vibration or ground induced longitudinal and lateral excitation due to runway unevenness. Neither of these vibrations is catastrophic, but still causes huge discomfort to pilots and passengers.
A. Shobana, M.Bala Ramamoorthy
openaire +2 more sources
Two-parameter bifurcation analysis of an aircraft nose landing gear model
Nonlinear Dynamics, 2021The Hopf–Hopf bifurcations of an aircraft nose landing gear model are investigated in this paper based on two pairs of continuation parameters. It is shown that due to the effect of higher-order terms, there exists a deviation between the bifurcation curve of the original system and the bifurcation curve of its truncated amplitude system, which results
Lifang Cheng, Hongjun Cao, Litao Zhang
openaire +2 more sources
Multidisciplinary modeling and analysis of nose landing gear shimmy
IET Conference ProceedingsXiying Chen +4 more
openaire +2 more sources
Nose landing gear strength test strain gauge vs FEA correlation
IET Conference ProceedingsWenmin Xu +3 more
openaire +2 more sources
Nose Landing Gear Door Re-design
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 2007Introduction The goal of this study was to re-design the F-22A Nose Landing Gear (NLG) Doors to reduce the cost. Cost was impacted by a) acquisition (fabrication methods) and b) installation and rigging time. There were additional requirements that also had to be satisfied: must be weight neutral +/1 pound, fit within the current NLG door opening ...
John Barnes +4 more
openaire +1 more source
Failure analysis of nose landing gear assembly
Engineering Failure Analysis, 2003Abstract This paper analyses the causes of the incident of an F-4 which landed abnormally due to a crack in the nose landing gear hydraulic actuator cylinder. Striations, typical of a fatigue crack, were observed on the fracture surface and a large quantity of corrosive oxide was detected in the initial stage of the crack.
Hong-Chul Lee +2 more
openaire +1 more source