Computation of subsonic and transonic flow about lifting rotor blades-Reference-Cited by-同舟云学术

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Computation of subsonic and transonic flow about lifting rotor blades

Published:1979-08-06 Issue: Volume: Page:
ISSN:
Container-title:5th Atmospheric Flight Mechanics Conference for Future Space Systems
language:
Short-container-title:

Author:

ARIELI R.¹,TAUBER M.¹

Affiliation:

1. NASA, Ames Research Center, Moffett Field, Calif.

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1979-1667

Reference9 articles.

1. 2aradonna, F. X."The Transonic Flow on a Helicopter Rotor," Ph.D. Dissertation,Stanford University, Mar. 1978.

2. r a n t , J. "Calculation of the Supercritical Flow Over the Tip Region of a Non-Lifting Rotor Blade a t Arbitrary Azimuth," Royal Aircraft Establishment Technical Report 77180,Dec. 1977.

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4. Use of Navier-Stokes code to predict flow phenomena near stall as measured on a 0.658-scale V-22 tiltrotor blade;20th Fluid Dynamics, Plasma Dynamics and Lasers Conference;1989-06-12

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