A calculator program for analyzing airloads on a wing of arbitrary planform and camber in subsonic flow /
John C. Sparks.

Description

Main Author

Sparks, John C.

Related Names

Air Force Flight Dynamics Laboratory (U.S.)
United States. Air Force.

Language(s)

English

Published

Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978.

Subjects

Camber (Aerofoils)
Aerofoils > Aerofoils / Computer programs.
Aerodynamic load > Aerodynamic load / Measurement > Aerodynamic load / Measurement / Computer programs.

Summary

A subsonic airloads program for small (8-K) calculators is presented. Features include good man-machine interaction and quick turn-around which speed preliminary design. The program is written in BASIC for the HP9830 or HP9831 calculator systems equipped with Matrix ROM and 9862A plotter. Programming techniques illustrated may be applied to any small system having special function keys or an equivalent capability. (Author).

Note

"Final report for period 1 April 1976 to 31 August 1976."
"January 1978."

Physical Description

vi, 48 pages: illustrations ; 28 cm

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