Lifting-Surface Theory of a Fully Submerged Hydrofoil

1965 ◽  
Vol 9 (01) ◽  
pp. 1-12
Author(s):  
Tetsuo Nishiyama

Lifting-surface theory of a fully submerged hydrofoil advanced at constant forward speed under the fixed submersion depth is developed, and then the properties of the lift and resistance are discussed in detail in relation with the effect of the Froude number. The disturbing velocity potential is, first of all, derived from the linearized condition on the free water surface. Then, from the boundary condition over the lifting surface, constructed on the Küchemann's conception, a basic integral equation is obtained for the distribution of circulation over the span, from which the lift-curve slope and the sum of the induced and wave-making resistance can be computed readily. This integral equation is solved by DeYoung and Harper's method. Comparisons of theoretical lift and resistance with the experimental data by NASA confirm the appropriateness of the construction of the present theory; and also the effects of the Froude number on the characteristics is definitely clarified. Damping and Inertia Coefficients for a Rolling or Swaying Vertical Strip 1Discussion by W. R. Porter2IN Table 2, of this paper, the author presents values of the damping constant for a vertical strip in horizontal (sway) oscillation for tabular values of nondimensional frequency. In the Addendum, he relates that another table, Table 3, was independently checked and found to vary only by 1 in the fourth decimal place. An unwary person may assume the same to be probably true for Table 2; and, therefore, the misprinted value at frequency 2.000 is hereby reported. The interval in the table at this frequency is sufficiently large that the irregular value may be otherwise undetected. Table 2 Table 3 In addition to correcting the misprint, the table as calculated by the writer at the Computation Center, MIT, presents confirmation that the original Table 2, except at 2.000, varies at most by 1 in the fourth decimal place. This new table provides entry at more closely spaced and more conventional frequencies with digit zero in the third decimal place. The new table also presents the wave-height ratio for convenience. The relation between wave-height ratio and damping constant is mentioned in the Addendum to the paper. To complete the presentation, a graph is shown here for the wave-height ratio for the vertical strip and also for the circular cylinder in horizontal (sway) oscillation as calculated by the writer. Fig. 01Wave-height ratio as a function of nondimensional frequency for vertical strip and circular cylinder in horizontal (sway) oscillation

1987 ◽  
Vol 31 (03) ◽  
pp. 151-163
Author(s):  
J. Leclerc ◽  
P. Salaun

A new lifting-surface theory is developed for the computation of three-dimensional hydrodynamic pressures on thin structures in the presence of a free surface. Two interesting cases are treated: the steady case and the supercritical unsteady case. The theory is linearized and the problem is reduced to the solution of an integral equation where the unknown function is the pressure difference between the elements of the structure and the right-hand side the angle of attack. Forces and moments are presented in both the steady and unsteady cases. This theory allows the analysis of flutter and the study of steady drag and of the turn of ships.


Author(s):  
G. F. Homicz ◽  
J. A. Lordi

A lifting-surface analysis is presented for the steady, three-dimensional, compressible flow through an annular blade row. A kernel-function procedure is used to solve the linearized integral equation which relates the unknown blade loading to a specified camber line. The unknown loading is expanded in a finite series of prescribed loading functions which allows the required integrations to be performed analytically, leading to a great savings in computer time. Numerical results are reported for a range of solidities and hub-to-tip ratios; comparisons are made with both two-dimensional strip theory and other three-dimensional results.


1975 ◽  
Vol 19 (04) ◽  
pp. 243-253
Author(s):  
W. van Gent

In an early stage of studies concerned with lifting-surface theory for ship screws, the Netherlands Ship Model Basin initiated the development of a numerical solution of the mathematical model. To achieve this, a rigorous method was followed consisting of separation of regular and singular parts of the kernel of the integral equation, preparation of numerical procedures for integration of the regular parts, and analytical integration of the singular parts. The general solution includes the steady load due to blade geometry in uniform flow, the unsteady load in nonuniform flow, and the unsteady load due to propeller vibrations. The pressure distribution in the chordwise direction is represented by a series of linear combinations of Chebyshev polynomials. In this paper an account is given of this method of solution.


AIAA Journal ◽  
1998 ◽  
Vol 36 ◽  
pp. 1788-1791
Author(s):  
Tetsuhiko Ueda

Author(s):  
Hidekazu Kodama ◽  
Masanobu Namba

A lifting surface theory is developed to predict the unsteady three-dimensional aerodynamic characteristics for a rotating subsonic annular cascade of swept blades. A discrete element method is used to solve the integral equation for the unsteady blade loading. Numerical examples are presented to demonstrate effects of the sweep on the blade flutter and on the acoustic field generated by interaction of rotating blades with a convected sinusoidal gust. It is found that increasing the sweep results in decrease of the aerodynamic work on vibrating blades and also remarkable reduction of the modal acoustic power of lower radial orders for both forward and backward sweeps.


AIAA Journal ◽  
1974 ◽  
Vol 12 (1) ◽  
pp. 28-37 ◽  
Author(s):  
KOJI ISOGAI

1964 ◽  
Author(s):  
H. ASHLEY ◽  
M. LANDAHL

1979 ◽  
Vol 30 (4) ◽  
pp. 529-543
Author(s):  
Shigenori Ando ◽  
Akio Ichikawa

SummaryApplications of “integral transforms of in-plane coordinate variables” in order to formulate unsteady planar lifting surface theories are demonstrated for both sub- and supersonic inviscid flows. It is concise and pithy. Fourier transforms are exclusively used, except for only Laplace transform in the supersonic streamwise direction. It is found that the streamwise Fourier inversion in the subsonic case requires some caution. Concepts based on the theory of distributions seem to be essential, in order to solve the convergence difficulties of integrals. Apart from this caution, the method of integral transforms of in-plane coordinate variables makes it be pure-mathematical to formulate the lifting surface problems, and makes aerodynamicist’s experiences and physical models such as vortices or doublets be useless.


2013 ◽  
Vol 48 (2) ◽  
pp. 246-252 ◽  
Author(s):  
Baris Bicer ◽  
Makoto Uchida

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