A Shorter Selection of Cases on the Conflict of Laws, by Joseph Henry Beale, Jr.Joseph Henry Beale1907
Report No. 602. Wind-tunnel and flight tests of slot-lip ailerons: by Joseph A. Shortal. 25 pages, illustrations, 23 × 29 cms. Washington, Government Printing Office, 1937. Price 15 centsJournal of the Franklin Institute1938PDF61 KB
Report no. 603, Wind-tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps: by Robert C. Platt and Joseph A. Shortal. 22 pages, illustrations, 23 × 29 cms. Washington, Government Printing Office, 1937. Price 10 centsJournal of the Franklin Institute1937PDF63 KB
National Advisory Committee for Aeronautics: Report No. 400. The Aerodynamic Characteristics of a Slotted Clark Y Wing as Affected by the Auxiliary Airfoil Position, by Carl J. Wenzinger and Joseph A. Shortal, 16 pages, illustrations, quarto. Washington, Superintendent of Documents, 1931.Price fifteen centsR. · Journal of the Franklin Institute1932PDF124 KB
Report No. 439, Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angels of Attack, V. Spoilers and Ailerons on Rectangular Wings: by Fred E. Weick and Joseph A. Shortal, 18 pages, illustrations, 23 × 29 cms. Washington, Superintendent of Documents, 1932. Price ten centsJournal of the Franklin Institute1932PDF67 KB
Report No. 444, Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angels of Attack. VI. Skewed Ailerons on Rectangular Wings: by Fred E. Weick and Joseph A. Shortal, 18 pages, illustrations, 23 × 29 cms. Washington, Superintendent of Documents, 1932. Price five centsJournal of the Franklin Institute1932PDF65 KB
National advisory committee for aeronautics: Report No. 427, The effect of multiple fixed slots and a trailing-edge Flap on the lift and drag of a clark Y airfoil: by Fred E. Weick and Joseph A. Shortal, 8 pages, illustrations, 23 × 29 cms. Washington, Superintendent of Documents, 1932Journal of the Franklin Institute1932PDF64 KB