Evaluation Of Helicopter Noise Due To B Blade Vortex Interaction For Five Tip Configurations
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Evaluation of Helicopter Noise Due to Blade-vortex Interaction for Five Tip Configurations
Author | : Danny R. Hoad |
Publisher | : |
Total Pages | : 84 |
Release | : 1979 |
Genre | : Acoustical engineering |
ISBN | : |
NASA Technical Paper
Author | : United States. National Aeronautics and Space Administration |
Publisher | : |
Total Pages | : 256 |
Release | : 1988 |
Genre | : Aeronautics |
ISBN | : |
Scientific and Technical Aerospace Reports
Author | : |
Publisher | : |
Total Pages | : 1460 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Helicopter Blade-vortex Interaction Locations
Author | : Danny R. Hoad |
Publisher | : |
Total Pages | : 112 |
Release | : 1987 |
Genre | : Rotors (Helicopters) |
ISBN | : |
High Performance Computing in Science and Engineering ‘13
Author | : Wolfgang E. Nagel |
Publisher | : Springer Science & Business Media |
Total Pages | : 689 |
Release | : 2013-12-12 |
Genre | : Computers |
ISBN | : 3319021656 |
This book presents the state-of-the-art in simulation on supercomputers. Leading researchers present results achieved on systems of the High Performance Computing Center Stuttgart (HLRS) for the year 2013. The reports cover all fields of computational science and engineering ranging from CFD via computational physics and chemistry to computer science with a special emphasis on industrially relevant applications. Presenting results of one of Europe’s leading systems this volume covers a wide variety of applications that deliver a high level of sustained performance. The book covers the main methods in high performance computing. Its outstanding results in achieving highest performance for production codes are of particular interest for both the scientist and the engineer. The book comes with a wealth of coloured illustrations and tables of results.
Helicopter Blade-vortex Interaction Locations: Scale-model Acoustics and Free-wake Analysis Results
Author | : Danny R. Hoad |
Publisher | : |
Total Pages | : 112 |
Release | : 1987 |
Genre | : |
ISBN | : |
The results of a model rotor acoustic test in the Langley 4- by 7-Meter Tunnel are used to evaluate a free-wake analytical technique. An acoustic triangulation technique is used to locate the position in the rotor disk where the blade-vortex interaction noise originates. These locations, along with results of the rotor free-wake analysis, are used to define the geometry of the blade-vortex interaction noise phenomena as well as to determine if the free-wake analysis is a capable diagnostic tool. Data from tests of two teetering rotor systems are used in these analyses. Keywords; Helicopter rotor disks; Free wake; Blade-vortex interactions; Acoustic properties.
Research and Technology Annual Report
Author | : Earth Resources Laboratory (U.S.) |
Publisher | : |
Total Pages | : 214 |
Release | : 1987 |
Genre | : Remote sensing |
ISBN | : |