Critical Mach numbers for thin untapered swept wings at zero incidence
1954
74 S.
Report
Englisch
DDC: | 629.13432 |
Critical Mach Number Prediction on Swept Wings
AIAA | 2017
|Theoretical supersonic wave drag of untapered sweptback and rectangular wings at zero lift
Engineering Index Backfile | 1947
|Critical Mach Number Prediction on Swept Wings (AIAA 2017-0266)
British Library Conference Proceedings | 2017
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