Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part I: Mach 5 and 8 Data for Expansion Corner Flows: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 63-679 Part 1

Development of a Low Altitude Turbulence Model for Estimating Gust Loads on Aircraft

Author(s): Lappe, U. O.
Corporate Author: New York University
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report Number: ASD TDR 63-318

Wind, wind Shear, and Gust design Criteria for Vertically-Rising Vehicles as Recommended on the Basis of Wind Data from Eleven United States and Foreign Locations

Author(s): Mazzola, L. L.
Corporate Author: AviDyne Research, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-06
Report Number: ASD TDR 62-908

Investigation of Techniques for Predicting the Development Cost and Development Time of Automatic Flight Control Systems

Author(s): Courtney, R. A.
Corporate Author: Planning Research Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 62-751

Simplified Analytical Methods for Use in Preliminary Design of Vertically-Rising Vehicles Subjected to Wind Shear Loads: Part II - Wind Statistics and Discrete Profiles

Author(s): Hobbs, N. P.
Corporate Author: AviDyne Research, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: FDL TDR 64-8 Part 2

Flat-Plate Boundary-Layer Transition at Hypersonic Speeds

Author(s): Deem, R. E.
Corporate Author: Douglas Aircraft Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Report Number: FDL TDR 64-129

Simplified Analytical Methods for Use in Preliminary Design of Vertically-Rising Vehicles Subjected to Wind Shear Loads: Part I - Evaluation of Methods

Author(s): Hobbs, N. P.
Corporate Author: AviDyne Research, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: FDL TDR 64-8 Part 1

Investigation of Dynamic Stability Derivatives of Vehicles Flying at Hypersonic Velocity

Author(s): Gilmore, Arthur
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 62-460