Journal ArticleDOI
The effect of displacement velocity on propeller performance
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This article is published in Journal of Aircraft.The article was published on 1983-08-01. It has received 4 citations till now. The article focuses on the topics: Advance ratio & Propeller.read more
Citations
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Journal ArticleDOI
Propeller aerodynamic performance by vortex-lattice method
Makoto Kobayakawa,Hiroyuki Onuma +1 more
TL;DR: In this paper, the vortex-lattice method is applied to rotating blades and the compressibility effect is included in the calculations through the Prandtl-Glauert similarity rule.
Journal ArticleDOI
Application of a panel code to unsteady wing-propeller interference
A. A. Rangwalla,L. N. Wilson +1 more
TL;DR: Attention is given to the predictions of unsteady, incompressible, potential flow, on the basis of an extension of Maskew's low-order paneling method, which is a nonlinear one in that the small-perturbation approximation is not made.
Journal ArticleDOI
Lift of an airfoil with a jet issuing from its surface
D. A. Tavella,K. Karamcheti +1 more
References
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Systematic Two-Dimensional Cascade Tests of NACA 65-Series Compressor Blades at Low Speeds
TL;DR: In this paper, the performance of NACA 65-series compressor blade sections in cascade has been investigated systematically in a low-speed cascade tunnel, and the results show that the performance is similar to that of the NACA 60-series.
Journal ArticleDOI
Characteristics of the wake behind a cascade of airfoils
R. Raj,B. Lakshminarayana +1 more
TL;DR: In this paper, an analytical and experimental investigation of the near and far wake characteristics of a cascade of airfoils is reported, which indicates that the wake is asymmetrical and this asymmetry is maintained even up to 3/4 chord length.
Proceedings ArticleDOI
The effect of blade sweep on propeller performance
TL;DR: In this paper, the induced flow-field vortex lattice methods are applied to a swept propeller blade for a high Mach number cruise, and the results of numerical calculations show that the power coefficient decreases as the blade is swept and the power loading distribution shifts inboard.
Journal ArticleDOI
Improved calibration method for a five-hole spherical Pitot probe
TL;DR: In this paper, a calibration method for a five-hole spherical Pitot probe by which the direction of a velocity vector is fixed by two Cartesian angles, one lying in the horizontal equatorial plane and the other in a vertical meridian plane containing the velocity vector, is described.
Journal ArticleDOI
The Effect of Reynolds Number and Turbulence Intensity on the Performance of a Compressor Cascade with Prescribed Velocity Distribution
J. Citavy,J. F. Norbury +1 more
TL;DR: In this paper, the effect of Reynolds number (Re) and turbulence intensity (Tu) on the aerodynamic performance of a PVD compressor cascade at design incidence was investigated. But the results were limited.
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