Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 956
Book Description
Scientific and Technical Aerospace Reports
Author: Reynolds Number Effects on the Performance of Lateral Control Devices
Author: Raymond E. MineckPublisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 148
Book Description
The influence of Reynolds number on the performance of outboard spoilers and ailerons was investigated on a generic subsonic transport configuration in the National Transonic facility over a chord Reynolds number range from 3x100000 to 30 x1000000 and a Mach number range from 0.50 to 0.94. Spoiler deflection angles of 0°, 10°, 15° and 20° and aileron deflection angles of -10°, 0° and 10° were tested. Aeroelastic effects were minimized by testing at constant normalized dynamic presuure conditions over intermediate Reynolds number ranges.
Cryogenic Wind Tunnels
Author: Marie H. TuttlePublisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 116
Book Description
Cryogenic Wind Tunnels: A Comprehensive, Annotated Bibliography
Author: Marie H. TuttlePublisher:
ISBN:
Category : Low temperature engineering
Languages : en
Pages : 146
Book Description
Monthly Catalog of United States Government Publications
Author: Monthly Catalogue, United States Public Documents
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1020
Book Description
NASA SP.
Author: Government reports annual index
Author: A Concept for Transition Mapping on a 10 Deg-cone in the National Transonic Facility Using Flow-pressure Variation
Author: Summary of Flow Modulation and Fluid-Structure Interaction Findings
Author: Wolfgang SchröderPublisher: Springer Science & Business Media
ISBN: 3642040888
Category : Technology & Engineering
Languages : en
Pages : 434
Book Description
The Collaborative Research Center SFB 401: Flow Modulation and Fluid-Structure Interaction at Airplane Wings investigates numerically and experimentally fundamental problems of very high capacity aircraft having large elastic wings. This issue summarizes the findings of the 12-year research program at RWTH Aachen University which was funded by the Deutsche Forschungsgemeinschaft (DFG) from 1997 through 2008. The research program covered the following three main topics of large transport aircraft: (i) Model flow, wakes, and vortices of airplanes in high-lift-configuration, (ii) Numerical tools for large scale adaptive flow simulation based on multiscale analysis and a parametric mapping concept for grid generation, and (iii) Validated computational design tools based on direct aeroelastic simulation with reduced structural models.