This paper presents a ALGOLprogram for calculating the thickness pressure distributions of arbitrary supersonic three dimensional wings by using the method of source singularities.
本文提供了用超音速源汇法计算任意三维机翼超音速厚度压强分布的算法语言程序。
2
The mathematical treatment has been justified in this paper and an ALGOL computational program is compiled.
文章证明了数学处理的合理性，并据此编制了ALGOL程序。
3
This paper introduces the ALGOL-60 program for pre-processing of dam observation data and its application, a flowchart and a demonstrating example of calculation is given.