Luo, Shijun; Cheng, Hsien K. Second-order small-disturbance solution for wing at supersonic speeds. (English) Zbl 0909.76040 AIAA J. 34, No. 12, 2562-2568 (1996). MSC: 76J20 76N15 PDFBibTeX XMLCite \textit{S. Luo} and \textit{H. K. Cheng}, AIAA J. 34, No. 12, 2562--2568 (1996; Zbl 0909.76040) Full Text: DOI
Cheng, H. K.; Luo, Shijun Transonic equivalence rule involving lift and shocks. (English) Zbl 0887.76032 AIAA J. 34, No. 5, 1080-1083 (1996). MSC: 76H05 PDFBibTeX XMLCite \textit{H. K. Cheng} and \textit{S. Luo}, AIAA J. 34, No. 5, 1080--1083 (1996; Zbl 0887.76032) Full Text: DOI
Cheng, H. K.; Emanuel, G. Perspective on hypersonic nonequilibrium flow. (English) Zbl 0829.76044 AIAA J. 33, No. 3, 385-400 (1995). Reviewer: O.Titow (Berlin) MSC: 76K05 76P05 76-02 82C21 PDFBibTeX XMLCite \textit{H. K. Cheng} and \textit{G. Emanuel}, AIAA J. 33, No. 3, 385--400 (1995; Zbl 0829.76044) Full Text: DOI
Cheng, H. K.; Meng, S. Y.; Chow, R.; Smith, R. C. Transonic swept wings studied by the lifting-line theory. (English) Zbl 0471.76072 AIAA J. 19, 961-968 (1981). MSC: 76H05 76B10 76-04 PDFBibTeX XMLCite \textit{H. K. Cheng} et al., AIAA J. 19, 961--968 (1981; Zbl 0471.76072) Full Text: DOI Link
Cheng, H. K.; Meng, S. Y. Lifting-line theory of oblique wings in transonic flows. (English) Zbl 0405.76031 AIAA J. 17, 121-124 (1979). MSC: 76H05 PDFBibTeX XMLCite \textit{H. K. Cheng} and \textit{S. Y. Meng}, AIAA J. 17, 121--124 (1979; Zbl 0405.76031) Full Text: DOI
Cheng, H. K. Lifting-line theory of oblique wings. (English) Zbl 0392.76044 AIAA J. 16, 1211-1213 (1978). MSC: 76G25 76B47 76B10 PDFBibTeX XMLCite \textit{H. K. Cheng}, AIAA J. 16, 1211--1213 (1978; Zbl 0392.76044) Full Text: DOI
Hafez, Mohammed M.; Cheng, H. K. Shock-fitting applied to relaxation solutions of transonic small- disturbance equations. (English) Zbl 0361.76060 AIAA J. 15, 786-793 (1977). MSC: 76H05 PDFBibTeX XMLCite \textit{M. M. Hafez} and \textit{H. K. Cheng}, AIAA J. 15, 786--793 (1977; Zbl 0361.76060) Full Text: DOI
Cheng, H. K. Lift corrections to transonic equivalence rule: Examples. (English) Zbl 0356.76043 AIAA J. 15, 366-373 (1977). MSC: 76H05 PDFBibTeX XMLCite \textit{H. K. Cheng}, AIAA J. 15, 366--373 (1977; Zbl 0356.76043) Full Text: DOI
Hafez, Mohamed M.; Cheng, H. K. Convergence acceleration of relaxation solutions for transonic flow computations. (English) Zbl 0356.76042 AIAA J. 15, 329-336 (1977). MSC: 76H05 76-04 PDFBibTeX XMLCite \textit{M. M. Hafez} and \textit{H. K. Cheng}, AIAA J. 15, 329--336 (1977; Zbl 0356.76042) Full Text: DOI
Cheng, H. K.; Lee, R. S. Freezing of dissociation and recombination in supersonic nozzle flows. I: General discussion and special analysis. II: More general analysis and numerical example. (English) Zbl 0159.57602 AIAA J. 6, 823-831, 831-837 (1968). PDFBibTeX XMLCite \textit{H. K. Cheng} and \textit{R. S. Lee}, AIAA J. 6, 823--831, 831--837 (1968; Zbl 0159.57602) Full Text: DOI
Cheng, Hsien K. Recent advances in hypersonic flow research. (English) Zbl 0107.20401 AIAA J. 1, 295-310 (1963). PDFBibTeX XMLCite \textit{H. K. Cheng}, AIAA J. 1, 295--310 (1963; Zbl 0107.20401) Full Text: DOI