Results 1 to 10 of about 34,676 (314)
Flutter/ASE Flight Test Risk Control Technique of Civil Fly-by-wire Aircraft
The existing research on flight test risk control techniques related to flutter/ASE test is not systematic enough,and has limited consideration of civil fly-by-wire aircraft characteristic and onboard flight test engineer.The flutter/ASE flight test risk
WANG Haigang, ZHANG Shaoyun
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This study explores the multidisciplinary design optimization (MDO) of the NASA Common Research Model (CRM) wingbox, utilizing both metallic and composite materials while addressing various constraints, including static strength, stiffness ...
Odeh Dababneh +2 more
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Flutter Boundary Prediction of a Two Dimensional Airfoil in Transonic Flight Regime with the Preset Angles of Attack [PDF]
Angle of attack has impact on transonic flow filed and aerodynamic force, but most of current researches on flutter use zero angle hypothesis, which has no consideration about angle of attack.
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Flutter analysis of mistuned bladed disks
Although bladed disks are nominally designed to be cyclically symmetric (tuned system), the vibration characteristics of all the blades on a disk are slightly different due to the manufacturing tolerance, deviations in the material properties, and wear during operation.
Yasutomo KANEKO +2 more
openaire +3 more sources
Experimental Methods Applied in a Study of Stall Flutter in an Axial Flow Fan
Flutter testing is an integral part of aircraft gas turbine engine development. In typical flutter testing blade mounted sensors in the form of strain gages and casing mounted sensors in the form of light probes (NSMS) are used.
John D. Gill +2 more
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Nonlinear Response Analysis of an Airfoil Using Multistep Differential Transform Method
The analysis of limit cycle oscillations (LCOs) and flutter behavior in hypersonic aeroelastic systems presents significant challenges owing to their strong nonlinearities. This study demonstrates the applicability of the Multistep Differential Transform
S. Shali, Jafarali Parol, S. R. Nagaraja
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Experimental and numerical study of dynamic characteristic of a complex all-movable rudder system
Modal analysis and flutter computation of a complex tail cabin system including six all-movable rudders for hypersonic flight vehicle was studied in this paper.
Yuguang Bai +3 more
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The nonlinear limit-cycle oscillations induced by aileron rotational freeplay are investigated by numerical simulation and flutter wind tunnel tests.
Yukai Sun +4 more
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Flutter is one of the most serious wind-induced vibration phenomena for long-span bridges and may cause the collapse of a bridge (e.g., the Old Tacoma Bridge, 1940).
Feng Wang +5 more
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AEROELASTIC FLUTTER ANALYSIS OF SUPERSONIC WING WITH MULTIPLE EXTERNAL STORES
: Flutter may be considered to be one of the most dangerous aeroelastic failure phenomenon. The flutter characteristic differs for each aircraft type, and depends on the wing geometry as well as its operational region of subsonic, transonic or supersonic
Nur Azam, Erwin Sulaeman
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