[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Cooper et al., 2008 - Google Patents

Optimization of a scaled SensorCraft model with passive gust alleviation

Cooper et al., 2008

Document ID
7903728733412280525
Author
Cooper J
Miller S
Sensburg O
Vio G
Publication year
Publication venue
12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference

External Links

Snippet

High altitude long endurance UAVs such as sensorcraft are extremely flexible and consequently are susceptible to excessive gust loads; therefore it is desirable to incorporate some form of gust load alleviation system into the air vehicle design. If successful, this could …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction
    • Y02T50/16Drag reduction by influencing airflow
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air-flow over aircraft surfaces, not otherwise provided for
    • B64C23/06Influencing air-flow over aircraft surfaces, not otherwise provided for by generating vortices
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/44Varying camber
    • B64C3/48Varying camber by relatively-movable parts of wing structures
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/80Technologies aiming to reduce green house gasses emissions common to all road transportation technologies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/10Shape of wings

Similar Documents

Publication Publication Date Title
Hui et al. Aerodynamic performance investigation on a morphing unmanned aerial vehicle with bio-inspired discrete wing structures
Bae et al. Aerodynamic and static aeroelastic characteristics of a variable-span morphing wing
Murua et al. Assessment of wake-tail interference effects on the dynamics of flexible aircraft
Gern et al. Structural and aeroelastic modeling of general planform wings with morphing airfoils
Communier et al. Experimental validation of a new morphing trailing edge system using Price–Païdoussis wind tunnel tests
Nguyen et al. Elastically shaped wing optimization and aircraft concept for improved cruise efficiency
Popov et al. Real time morphing wing optimization validation using wind-tunnel tests
Raveh Gust-response analysis of free elastic aircraft in the transonic flight regime
Van Zyl et al. Aeroelastic analysis of T-tails using an enhanced doublet lattice method
Murua et al. T-tail flutter: Potential-flow modelling, experimental validation and flight tests
Wei et al. Numerical study of a supercritical airfoil/wing with variable-camber technology
Goates et al. Practical implementation of a general numerical lifting-line method
Dehaeze et al. Mesh deformation method for rotor flows
Cooper et al. Optimization of a scaled SensorCraft model with passive gust alleviation
Yang et al. Aeroelastic trim and flight loads analysis of flexible aircraft with large deformations
Chen et al. Overset Euler/Boundary-Layer solver with panel-based aerodynamic modeling for aeroelastic applications
Murua et al. Open-loop stability and closed-loop gust alleviation on flexible aircraft including wake modeling
Nguyen et al. Aeroelastic analysis of a flexible wing wind tunnel model with variable camber continuous trailing edge flap design
Kier An integrated flexible aircraft model for optimal control surface scheduling of manoeuvre load alleviation and wing shape control functions
Ting et al. Aerodynamic load analysis of a variable camber continuous trailing edge flap system on a flexible wing aircraft
Miller et al. Development of an adaptive wing tip device
Soneda et al. Multi-fidelity aeroelastic simulation of a morphing wing trailing edge
Nguyen et al. Aeroelastic analysis of wind tunnel test data of a flexible wing with a variable camber continuous trailing edge flap (VCCTEF)
Castrichini Parametric Assessment of a Folding Wing-Tip Device for Aircraft Loads Alleviation
Murua et al. Stability and open-loop dynamics of very flexible aircraft including free-wake effects