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Integrated Effects of Environmental and Classroom Noise on Attention and Learning in School-age Children.

Noise Health
Badea DO, Darabont DC, Cioca LI, Coman C, Chis TV.   +4 more
europepmc   +1 more source

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Full-scale aircraft impact test for evaluation of impact force

Nuclear Engineering and Design, 1993
Abstract Previously, estimates of the force caused by aircraft impact into rigid structures have been determined using theoretical methods based on the aircraft's calculated mass and strength distribution. However, these methods required many assumptions to be made and they left many questions unanswered.
T. Sugano, H. Tsubota, Y. Kasai, N. Koshika, S. Orui, W.A. von Riesemann, D.C. Bickel, M.B. Parks   +7 more
openaire   +3 more sources

Analytic extrapolation to full-scale aircraft dynamics

Journal of Aircraft, 1982
T extrapolation from subscale wind-tunnel data to fullscale flight becomes an especially serious problem at subsonic speeds when stall is involved and at high subsonic and transonic speeds where shock boundary-layer interaction can dominate the aerodynamics.
L. ERICSSON, J. REDING
openaire   +1 more source

Full-scale aircraft tire pressure tests

2009
This paper describes an outdoor full-scale test planned to improve experimental and theoretical knowledge related to the effects of aircraft internal tire inflation pressure on the behavior and damage of flexible pavement. Since modern aircraft can have tire pressures greater than 15 bar, the tests will focus on pressures from 15 bar to 17.5 bar.
Fabre, C., Balay, Jean Maurice, Lerat, P., Mazars, A.   +3 more
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Full-scale static test of small composite aircraft

Advanced Composite Materials, 2013
This paper addresses the accuracy of test load application and reaction prediction of aircraft full-scale static test.
Jae-Yeul Shim, Seokmin Ahn
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Full Scale Test of a Transport Aircraft Thrust Vectoring System

SAE Technical Paper Series, 1997
<div class="htmlview paragraph">VSTOL transport aircraft pose unique thrust vectoring control requirements. The control moments have to be very large in comparison with VSTOL fighter aircraft because the moments of inertia are so much larger due to a high aspect ratio wing and distributed payload in the fuselage.
Anthony duPont, Anthony duPont
openaire   +2 more sources