Case study on aero elasticity
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Transcript of Case study on aero elasticity
SIDDARTHA INSTITUTE OF
SCIENCE AND TECHNOLOGYPowerPoint presentation
on Case study on Aero
ElasticityBy
SANJANA P U
Aero elasticity is the study of the interaction of inertial, structural and aerodynamic forces on aircraft, buildings, surface vehicles etc.
INTRODUCTION
FIGURE : COLLARS TRIANGLE
AERO ELASTICITY
STATIC AEROELASTICITY
DIVERGENCE
CONTROL REVERSA
L
DYNAMIC AEROELASTICITY
FLUTTER BUFFETING TRANSONIC
Elastic twist of the wing suddenly becoming theoretically infinite
Phenomenon occurring only in wings with ailerons or other control surfaces, where control surfaces reverse their usual functionality
DIVERGENCE:
CONTROL REVERSAL:
STATIC AEROELASTICITY
Dynamic instability
FLUTTER:DYNAMIC AEROELASTICITY
BUFFETING: A high-frequency instability
Shock Waves
CASE STUDYBoeing X-53 Active Aero elastic Wing
First flight -8 December 2006 Role -Technology Demonstrator National origin -United States Manufacturer -McDonnell Douglas
Northrop Corporation
Active Aero elastic Wing
1 Design and development
Integrates wing aerodynamics, controls, and structure to harness and control wing aero elastic twist at high speeds and dynamic pressures.
Technology
An aircraft maneuvers - deploying flight control surfaces into the airflow, which modify the lift of the surface they are attached to.
1.1 Aero elasticity and controls
1.2 AAW testing1. Taking an existing F/A-18 airframe2. Modified with a preproduction pre roll
mod wing3. Added an outboard leading edge flap drive
system and an updated flight control computer
2 SpecificationsGeneral characteristics Crew: 1 Wingspan: 38 ft 5 in (11.71 m) Height: 15 ft 3 in (4.65 m) Max takeoff weight: 39,000 lb (17,690 kg) Power plant: 2 × General Electric F404-GE-400 low-
bypass turbofan engines, 16,000 lbf (71 KN) thrust each
Performance Maximum speed: 1,032 KN; 1,912 km/h (1,188
mph) Service ceiling: 50,000 ft (15,000 m)
Avionics
Aero elastic twist can be controlled Enables the use of high aspect ratio, thin,
swept wings Provide excellent high speed rolling
performance No additional stiffness was added for static
aero elastic issues Overall control authority is affected
Merits & Demerits
THANK YOU