Zobrazeno 1 - 10
of 25
pro vyhledávání: '"Leroy H. Smith"'
Autor:
Alan Roy Stuart, Leroy H. Smith, Jan Christopher Schilling, Guy Cliff Murphy, Bruce J. Gordon
Publikováno v:
The Journal of the Acoustical Society of America. 94:3535-3535
The invention concerns reduction of tip vortices in aircraft propellers, wherein a fence having anhedral or dihedral is attached to the blades of the propeller. Another form of the invention is applicable to counterrotating propeller systems, wherein
Autor:
C. C. Koch, Leroy H. Smith
Publikováno v:
Journal of Engineering for Power. 98:411-424
A method is presented for calculating the design point efficiency potential of a multistage compressor. Design parameters that affect the efficiency are vector diagram shape, aerodynamic loading level, aspect ratio, solidity, clearances, airfoil maxi
Autor:
Leroy H. Smith, G. G. Adkins
Publikováno v:
Journal of Engineering for Power. 104:97-110
Flow measurements taken in multistage axial-flow turbomachines suggest that substantial spanwise mixing of flow properties often occurs. In addition, measured blade row turnings often show considerable deviation from two-dimensional cascade theory, p
Autor:
Leroy H. Smith
Publikováno v:
Journal of Turbomachinery. 109:313-324
A method being used to design unducted fans, which are counterrotating propellers with unusually high disk loadings, is described. The quasi-three-dimensional approach employed is similar to that used for ducted fan designs; it consists of a circumfe
Autor:
Hsuan Yeh, Leroy H. Smith
Publikováno v:
Journal of Basic Engineering. 85:401-414
An approximate method for including the effects of sweep and dihedral when designing axial-flow turbomachinery blading is presented. Blades are said to have sweep when the flow direction is not perpendicular to the spanwise direction, and dihedral wh
Autor:
Leroy H. Smith
Publikováno v:
Journal of Fluids Engineering. 80:517-523
Certain types of axial-flow-compressor stage designs have the ability to add extra energy to high-loss regions of the inlet flow and thereby tend to smooth out inlet-flow distortion rapidly. A recovery ratio, which is believed to give a quantitative
Autor:
Leroy H. Smith
Publikováno v:
Journal of Engineering for Power. 88:1-12
An equation is derived that describes the radial variation of circumferential-average flow properties inside of a turbomachine blade row. A physical interpretation is given for each of the several terms in the equation, and the magnitudes of the term
Autor:
Leroy H. Smith
Publikováno v:
Journal of Basic Engineering. 82:726-728
Autor:
Leroy H. Smith
Publikováno v:
Journal of Basic Engineering. 88:688-690
The motion of a wake as it passes through a blade row that moves relative to the wake generator is considered. Viscosity is neglected, and it is shown that the wake is modified by a chopping process that disperses it and also by uneven energy additio
Autor:
Leroy H. Smith
Publikováno v:
Journal of Basic Engineering. 81:398-400