Box 2
Contains 42 Results:
Standards for Discharge Measurement with Standardized Nozzles and Orifices, 1940-09
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
Flow Over a Slender Body of Revolution at Supersonic Velocities (Robert T. Jones and Kenneth Margolis), 1946-08
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
Characteristics of Flow Over Inclined Bodies of Revolution (H. Julian Allen and Edward W. Perkins), 1951-03-05
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
Three-Dimensional Airfoils, 1957-08
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
Discontinuous Flows and Free Streamline Solutions for Axisymmetric Bodies at Zero and Small Angles of Attack (Heinz G. Struck), 1970
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
Analytical Determination of Pressure Distributions on Blunt-Based Bodies of Revolution Under Influence of the Wake, at Small Angles of Attack in Subsonic Flow by the Use of Surface Singularities (Heinz G. Struck), 1964-07-10
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
Description of a Program for Calculating the Subsonic Lift Distribution of a Wing of Arbitrary Planform, 1964-11-18
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
Extension of the One-Dimensional, Time-Dependent Method of Characteristics to the Flow in a Tube Wind Tunnel with Mass Extraction (H.G. Struck)
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
Application of the Characteristic Method in Calculating the Time Dependent, One-Dimensional, Compressible Flow in a Tube Wind Tunnel (Heinz G. Struck and John D. Warmbrod), 1968-08-21
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
Discontinuous Flows and Free Streamline Solutions for Axisymmetric Bodies at Zero and Small Angles of Attack, 1970-02
Documents relating to Heinz Struck's career with NASA, SAIC, and BD.
