Contrails
The goal of the Contrails project is to help preserve and disseminate the technical record of 20th century aerospace research, highlighting in particular the research endeavors of the Illinois Tech community.

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8 reports

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
full text unavailable

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

Author(s): U. O. Lappe; R. H. Thuillier; R. W. Reeves
Corporate Author: New York University
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-07
Report Number: ASD TDR 63-318
full text unavailable

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): L. L. Mazzola; J. Putukian; E. S. Criscione; N. P. Hobbs
Corporate Author: AviDyne Research, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-06
Report Number: ASD TDR 62-908
full text unavailable

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

Author(s): R. A. Courtney; H. M. Dye; R. L. Erler; C. P. Martin; F. C. Reed; H. T. Spiro; D. E. Johnston
Corporate Author: Planning Research Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 62-751
full text unavailable

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

Flat-Plate Boundary-Layer Transition at Hypersonic Speeds

Author(s): R. E. Deem; C. R. Erickson; J. S. Murphy
Corporate Author: Douglas Aircraft Company
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-10
Report Number: FDL TDR 64-129
full text unavailable

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

Author(s): N. P. Hobbs; E. S. Criscione; M. Ayvazian
Corporate Author: AviDyne Research, Inc.
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report Number: FDL TDR 64-8 Part 1
full text unavailable

Investigation of Dynamic Stability Derivatives of Vehicles Flying at Hypersonic Velocity

Author(s): Arthur Gilmore, Vladimir Seredinsky and Donald MacKenzie
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report Number: ASD TDR 62-460
full text unavailable