1-2-3. |
4-5-6. |
7-8-9. |
10-11-12. |
16-17. |
21-22-23. |
24-25-26. |
34-35-36. |
40-41-42. |
43-44-45. |
100. |
106. |
107. |
108. |
109. |
110. |
111. |
158-159-160. |
200-201-202. |
250-251-252. |
300-301-302. |
350-351-352. |
312-313-314. |
362-363-364. |
315-316-317. |
365-366-367. |
318-319-320. |
368-369-370. |
321-322-323. |
371-372-373. |
324-325-326. |
327-328-329. |
340-341-342. |
374-375-376. |
383-384-385. |
386-387-388. |
400-401-402. |
450-451-452. |
521. |
522. |
523. |
524. |
525. |
526. |
527. |
528. |
529. |
530. |
531. |
581. |
650. |
661. |
662. |
663. |
670. |
680. |
690. |
691. |
692. |
701. |
703. |
705. |
708. |
709. |
715. |
718. |
720. |
721. |
722. |
723. |
725. |
751-752. |
754. |
755-756. |
800. |
801. |
802. |
803. |
804. |
805. |
806. |
807. |
808. |
812. |
813. |
814. |
815a-b-c. |
816. |
819. |
820. |
821. |
822. |
826. |
827. |
830. |
833. | 833: Aerodynamics: |
834. |
835. |
860. |
863. |
866. |
867-868. |
869. |
885. |
900. |
901. |
902. |
903. |
904. |
905. |
906. |
907. |
908. |
909. |
910. |
911-912. |
916-917-918. |
920. |
925. |
930-931-932. |
940-941-942. |
950-951. |
952-953-954-955. |
956. |
960-961. |
966-967-968. |
975. |
980-981. |
990-991-992. |
The University of Virginia record February 1, 1936 | ||
833: Aerodynamics:
9:30-10:30, T. Th. S.
Aerodynamic theory, including consideration of circulatory and vortex
flow. Theory of wing section and of complete wings. Aerodynamic design
of an airplane to satisfy assigned specifications, including balance, control,
performance, and stability. (Fall.)
Assistant Professor Morse.
The University of Virginia record February 1, 1936 | ||