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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6 reports

An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. I. Surface Pressure Distributions on a Blunted Flat Plate

Author(s): G. M. Gregorek; T. C. Nark; J. D. Lee
Corporate Author: Ohio State University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-03
Report Number: ASD TDR 62-792 Volume 1
full text by request

An Experimental Investigation of the Surfact Pressure and the Laminar Boundary Layer on a Blunt Flat Plate in Hypersonic Flow: Vol. II. Laminar Boundary Layer Profile on the Flat Plate

Author(s): G. M. Gregorek; T. C. Nark; J. D. Lee
Corporate Author: Ohio State University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-03
Report Number: ASD TDR 62-792 Volume 2
full text by request

NB-66B High Altitude Gust Survey Technical Analysis, Volume I.

Author(s): J. A. Strom and T. G. Weathermon
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-04
Report Number: ASD TDR 63-145 Volume 1
full text by request

NB-66B High Altitude Gust Survey Power Spectra, Volume II.

Author(s): J. A. Strom and T. G. Weathermon
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-04
Report Number: ASD TDR 63-145 Volume 2
full text by request

NB-66B High Altitude Gust Survey Time Series, Volume III.

Author(s): J. A. Strom and T. G. Weathermon
Corporate Author: Douglas Aircraft Company, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-04
Report Number: ASD TDR 63-145 Volume 3
full text by request

Fixed-Base Simulator Investigation of the Effect of L (sub alpha) and True Speed on Pilot Opinion of Longitudinal Flying Qualities

Author(s): Charles R. Chalk
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1963-11
Report Number: ASD TDR 63-399
full text by request