The information below was obtained from http://jarnonieuwenhuize.nl/HBA/Index_NACA_Publications.pdf
1. Carl J. Wenzinger and Thomas A. Harris; Wind tunnel force tests in wing systems through large angles of attack; naca-tn-294 (August 1928)
2. Carl J. Wenzinger and Oscar Loeser, Jr.; Wind tunnel pressure distribution tests on an airfoil with trailing edge flap; naca-tn-326 (October 1929)
3. Montgomery Knight and Carl J. Wenzinger; The effect of wing tip floating ailerons on the autorotation of a monoplane wing model; naca-tn-336 (March 1930)
4. Montgomery Knight and Carl J. Wenzinger; Wind-tunnel tests on a series of wing models through a large angle of attack range. Part I : force tests; naca-report-317 (1930)
5. Carl J. Wenzinger and Thomas A. Harris; The vertical wind tunnel of the National Advisory Committee for Aeronautics; naca-report-387 (February 1931)
6. Fred E. Weick and Carl J. Wenzinger; Preliminary investigation of rolling moments obtained with spoilers on both slotted and plain wings; naca-tn-415 (April 1932)
7. Fred E. Weick and Carl J. Wenzinger; Effect of length of Handley Page tip slots on the lateral-stability factor, damping in roll; naca-tn-423 (July 1932)
8. Carl J. Wenzinger; Pressure distribution over a thick, tapered and twisted monoplane wing model-NACA 81-J; naca-report-367 (1932)
9. Montgomery Knight and Carl J. Wenzinger; Rolling moments due to rolling and yaw for four wing models in rotation; naca-report-379 (1932 )
10. Carl J. Wenzinger and Joseph A. Shortal; The aerodynamic characteristics of a slotted Clark y wing as affected by the auxiliary airfoil position; naca-report-400 (1932)
11. Fred E. Weick and Carl J. Wenzinger; Wind tunnel research concerning lateral control devices, particularly at high angles of attack VII : Handley Page tip and full-span slots with ailerons and spoilers; naca-tn-443 (January 1933)
12. Fred E. Weick and Carl J. Wenzinger; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack IX : tapered wings with ordinary ailerons; naca-tn-449 (February 1933)
13. Carl J. Wenzinger; The effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing; naca-tn-472 (September 1933)
14. Fred E. Weick and Carl J. Wenzinger; The characteristics of a Clark y wing model equipped with several forms of low-drag fixed slots; naca-report-407 (1933)
15. Fred E. Weick and Carl J. Wenzinger; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack I : ordinary ailerons on rectangular wings; naca-report-419 (1933)
16. Fred E. Weick and Carl J. Wenzinger; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack III : ordinary ailerons rigged up 10 degrees when neutral; naca-report-423 (1933)
17. Carl J. Wenzinger; Wind-tunnel measurements of air loads on split flaps; naca-tn-498 (May 1934)
18. Carl J. Wenzinger; The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing; naca-tn-505 (September 1934)
19. Fred E. Weick and Carl J. Wenzinger; Wind-tunnel research comparing lateral control devices, particularly at high angles of attack XII : upper-surface ailerons on wings with split flaps; naca-report-499 (1935)
20. Carl J. Wenzinger; Pressure distribution over a Clark Y-H airfoil section with a split flap; naca-tn-627 (December 1937)
21. Carl J. Wenzinger; Wind-tunnel investigation of the aerodynamic balancing of upper-surface ailerons and split flaps; naca-report-549 (1937)
22. Carl J. Wenzinger; Wind-tunnel investigation of ordinary and split flaps on airfoils of different profile; naca-report-554 (1937)
23. Carl J. Wenzinger and Thomas A. Harris; Pressure distribution over a rectangular airfoil with a partial-span split flap; naca-report-571 (1936)
24. Carl J. Wenzinger; Pressure distribution over an airfoil section with a flap and tab; naca-report-574; (1936)
25. Carl J. Wenzinger; Wind-tunnel investigation of tapered wings with ordinary ailerons and partial-span split flaps; naca-report-611 (1937)
26. Carl J. Wenzinger; Pressure distribution over an NACA 23012 airfoil with an NACA 23012 external-airfoil flap; naca-report-614 (1938)
27. Carl J. Wenzinger and Walter B. Anderson; Pressure distribution over airfoils with Fowler flaps; naca-report-620 (1938)
28. Carl J. Wenzinger and James B. Delano; Pressure distribution over an NACA 23012 airfoil with a slotted and a plain flap; naca-report-633 (1938)
29. Carl J. Wenzinger; Wind-tunnel tests of a Clark Y wing having split flaps with gaps; naca-tn-650; (May 1938)
30. Carl J. Wenzinger, and Millard J. Bamber; Wind-tunnel of three lateral-control devices in combination with a full-span slotted flap on an NACA 23012 airfoil; naca-tn-659 (August 1938)
31. Carl J. Wenzinger and Milton B. Ames, Jr; Wind-tunnel investigation of rectangular and tapered NACA 23012 wings with plain ailerons and full-span split flaps; naca-tn-661 (August 1938)
32. Carl J. Wenzinger Wenzinger and Francis M. Rogallo; Resume of air-load data on slats and flaps; naca-tn-690 (March 1939)
33. Carl J. Wenzinger and Thomas A. Harris; Wind-tunnel investigation of an NACA 23012 airfoil with various arrangements of slotted flaps; naca-report-664 (1939)
34. Carl J. Wenzinger and Thomas A. Harris; Wind-tunnel investigation of NACA 23012, 23021, and 23030 airfoils with various sizes of split flap; naca-report-668 (1939)
35. Carl J. Wenzinger and Thomas A. Harris; Wind-tunnel investigation of NACA 23012 airfoil with various arrangements of slotted flaps; naca-report-677 (1939)
36. Carl J. Wenzinger and William E. Gauvain; Wind-tunnel investigation of an NACA 23012 airfoil with a slotted flap and three types of auxiliary flap; naca-report-679 (1939)
37. Carl J. Wenzinger and Thomas A. Harris; Preliminary wind-tunnel investigation of an NACA 23012 airfoil with various arrangements of venetian-blind flaps; naca-report-689 (1940)
38. Carl J. Wenzinger and John D. Bowen; Tests of round and flat spoilers on a tapered wing in the NACA 19-foot pressure wind tunnel; naca-tn-801 (March 1941)
39. Carl J. Wenzinger and Francis M. Rogallo; Wind-tunnel investigation of spoiler, deflector, and slot lateral-control devices on wings with full-span split and slotted flaps; naca report-706 (1941)