Papers Presented at the Symposium on Control and Stability at Supersonic Speeds Held June 19 and 20, 1946

摘要

Contents: Aerodynamically Similar Models for Testing Jet-Propelled Missiles, by H. J. Stewart, California Institute of Technology; Supersonic Conical Flow Theory, by Leon Beskin, Consolidated Vultee Aircraft Coporation; Launching Problems of the RTV, by R. B. Hullett, Cornell Aeronautical Laboratory; Two-Dimensional Missile Trajectory, by G. C. Munro, Applied Physics Laboratory, The Johns Hopkins University; The Motion of Uncontrolled Nonspinning Missiles, by J. B. Rosser, Cornell University; Wind Tunnel and Flight Tests for Bumblebee, by A. R. Eaton, Applied Physics Laboratory, The Johns Hopkins University; Dynamic Stability at Supersonic Speed, by M. V. Barton, Defense Research Laboratory, University of Texas; The CTV Beam Rider, by D. T. Sigley, Applied Physics Laboratory, The Johns Hopkins University; Stability and Guidance, by E. L. Norton, Bell Telephone Laboratories; The Dynamic Response of a Missile to Specified Guidance Signals, by D. Young, Defense Research Laboratory, University of Texas; Control and Stability, by G. H. Stoner, Boeing Aircraft Company; Problems Involved in STV Flight Test Program, by A. Sowyrda, Cornell Aeronautical Laboratory; and List of Representatives Attending The Symposium On Control And Stability At Supersonic Speeds.