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Preliminary Study of a Wing-tip Vortex Using Laser Velocimetry

Preliminary Study of a Wing-tip Vortex Using Laser Velocimetry PDF Author: R. K. Takahashi
Publisher:
ISBN:
Category : Vortex-motion
Languages : en
Pages : 40

Book Description


Preliminary Study of a Wing-tip Vortex Using Laser Velocimetry

Preliminary Study of a Wing-tip Vortex Using Laser Velocimetry PDF Author: R. K. Takahashi
Publisher:
ISBN:
Category : Vortex-motion
Languages : en
Pages : 40

Book Description


Preliminary Study of a Wing-tip Vortex Using Laser Velocimetry

Preliminary Study of a Wing-tip Vortex Using Laser Velocimetry PDF Author: R. K. Takahashi
Publisher:
ISBN:
Category : Vortex-motion
Languages : en
Pages : 40

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 710

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1006

Book Description


Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1690

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 728

Book Description


STAR

STAR PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 920

Book Description


AIAA Journal

AIAA Journal PDF Author: American Institute of Aeronautics and Astronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1024

Book Description


Preliminary Investigation of the Role of the Tip Vortex in Rotary Wing Aerodynamics Through Flow Visualization

Preliminary Investigation of the Role of the Tip Vortex in Rotary Wing Aerodynamics Through Flow Visualization PDF Author: R. W. Hale
Publisher:
ISBN:
Category :
Languages : en
Pages : 39

Book Description
The interaction between the tip vortices and successive rotor blades is responsible for two important helicopter problems, static loss in lift and blade slap during power descent. As a step toward the solution of these problems, the objective of this investigation was to examine the flowfield about an isolated blade in rectilinear flow up to 40 chords downstream. Wind tunnel tests were carried out on the tip section of a HR2S-1 (S-56) blade in the NASA Langley V/STOL Research Wind Tunnel. Visualization of the detailed flow patterns, particularly the tip vortex and rollup in the near wake, was achieved using small, neutrally-buoyant bubbles as flow tracers. To provide adequate illumination, a new, expanded lighting arrangement was assembled from an array of searchlights. Also, a special chopper unit was designed and constructed for quantitative velocity data. Records of the flow patterns were made, both by means of still photography and a video system employing a high-sensitivity camera. (Author).

Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 726

Book Description