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44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference | 2003

Flutter Characteristics of an Over-the-Wing Engine Mount Business-Jet Configuration

Michimasa Fujino; Hiroki Oyama; Hideo Omotani

Mounting engines on the wing causes complex wing flutter characteristics. The location of the engine mass and the stiffness of the pylon relative to the wing are important in preventing hazardous wing flutter. In addition, if the nacelles are installed over the wing, aerodynamic interference between the wing and the nacelle may cause unfavorable flutter characteristics, in particular, at transonic speeds. The flutter characteristics of an over-the-wing engine mount configuration obtained from theoretical analyses and low speed and transonic wind tunnel tests, are presented. Nomenclature c wing local chord b wing semi-chord at 75% wing span D di ssipation function g structural damping gi structural damping for ith mode k reduced frequency


Archive | 2002

Model for wind tunnel test

Hideo Omotani; Hiroki Oyama; Masaki Kobayashi


Archive | 2009

Pedal operated apparatus for controlling an aircraft nose wheel steering system

Hiroki Oyama; Michimasa Fujino


Archive | 2009

HYDRAULIC SYSTEM FOR AIRCRAFT

Hiroki Oyama


Archive | 2011

Variable gain control nose wheel steering system

Hiroki Oyama


Archive | 2008

Aircraft brake system

Charles T. O'Connell; Hiroki Oyama


Archive | 2010

Shut-off valve for hydraulic system

Hiroki Oyama; Michael Joseph Boland


Archive | 2011

Aircraft brake handle assembly

Hiroki Oyama; Katsutoshi Tada; Charles T. O'Connell


Archive | 2009

AERODYNAMIC BRAKING DEVICE FOR AIRCRAFT

Hiroki Oyama


Archive | 2011

Brake control assembly plane

Hiroki Oyama; Katsutoshi Tada; Charles T. O'Connell

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