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Journal ArticleDOI

Drop Testing Naval Aircraft and the VSD Landing Gear Dynamic Test Facility

C. C. Daughetee
- 01 Dec 1974 - 
- Vol. 11, Iss: 12, pp 758-764
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TLDR
In this paper, the authors describe a laboratory facility developed by Vought Systems Division (VSD) of LTV Aerospace Corp. and techniques used to realistically simulate landings of full scale aircraft under precisely controlled conditions.
Abstract
This paper describes a laboratory facility developed by Vought Systems Division (VSD) of LTV Aerospace Corp. and techniques used to realistically simulate landings of full scale aircraft under precisely controlled conditions. Capabilities are included to evaluate effects of running over deck obstructions during carrier landings or other types of bumps that might be encountered in rough field operations of aircraft. The project provided VSD with the most accurate method known for dynamic simulation of aircraft landings and safe evaluation of the structural adequacy of airframes and landing gear systems for landing loads. Operational characteristics of the facility are predictable and repeatable. A deck obstruction or bump can be repeatedly passed under the landing gear wheel within */2 in. of any preselected point in the stroke of a landing gear strut at any sink speed or landing velocity to 120 knots. Tests performed in the facility have shown that running over a bump can increase both main gear and nose gear loads significantly and can also result in tires being cut and rims bent at lower sink speeds than previously anticipated. Comparison of data shows the laboratory data to be characteristic of flight test data.

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Citations
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Journal ArticleDOI

A method for determining the horizontal impact load based on the rotational speed of the aircraft's wheel in a landing gear drop test

TL;DR: The maximum horizontal impact load experienced by an aircraft's landing gear wheel during landing is an important parameter in the landing gear's safety design and performance analysis using a non-linear model as mentioned in this paper.
Journal ArticleDOI

Experimental rig to estimate the coefficient of friction between tire and surface in airplane touchdown simulations

TL;DR: A filtering method that is based on the ensemble empirical mode decomposition and the bandwidth of probability density function of each intrinsic mode function to extract friction and impact force signals is developed and the coefficient of friction is calculated.
Proceedings ArticleDOI

An overview of researches on deck-landing of carrier-based aircrafts

TL;DR: The major focus of the paper was to summarize work documented from the previous decades and to highlight the latest efforts in solving these problems, as well as try to highlight a new trail in designs of auxiliary shiplanding device.
Book ChapterDOI

Dynamics of Articulated Landing Gear in Tail-Down Landing Condition

TL;DR: In this paper, the dynamics of the articulated main landing gear, during level and tail-down landing conditions, using MSC/ADAMS software were compared with the available landing gear analysis program, which has been experimentally validated by the drop tests.