A general method for determining the aerodynamic characteristics of fan-in-wing configurations.

Description

Related Names

Wallace, R. E., author.
Standen, N. M., author.
Scholey, M. B., author.
Saaris, G. R., author.
Rubbert, P. E., author.
Sundstrom, K. A., author.
Gilbert, R. F., author.
Hink, G. R., author.
U.S. Army Aviation Materiel Laboratories.
Boeing Company

Language(s)

English

Published

Fort Eustis, Virginia, U.S. Army Aviation Materiel Laboratories, 1967.

Subjects

Aerodynamics > Aerodynamics / Mathematical models.
Aerodynamics.
Aerodynamics > Aerodynamics / Mathematical models.
Aerodynamics.

Summary

The report describes a digital computer program developed to study the aerodynamic characteristics of fan-in-wing configurations. The program is written in the FORTRAN IV and ASCENT languages for the Control Data Corporation 6000-series digital computers. Three basic packages are provided by the program: a geometry package produces a detailed description of the configuration, an aerodynamic package provides a theoretical solution for the potential flow about the configuration, and a boundary-layer package furnishes the boundary-layer characteristics on the wing surface. The report provides a description of the program, flow charts and segmentation structure diagrams, and input data formats.

Note

[Prepared by Boeing Company, Renton, Wash.].
(Task 1F125901A14234, contract DA 44-177-AMC-323(T).).
4to.
Dec. 1967.

Physical Description

2 volumes

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