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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11 reports

Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 1: Model Design And Testing Techniques

Author(s): John F. McCarthy, Jr. , Gifford W. Asher, John S. Prigge, Jr. , Gilbert M. Levy
Corporate Author: Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report Number: WADC TR 54-113 Part 1
full text available

Theoretical Investigation Of Optimum Pressures In Aircraft Hydraulic Systems

Author(s): Conrad H. Cooke, Eugene Gessner, Robert L. Smith
Corporate Author: Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1954-01
Report Number: WADC TR 54-189 Volume 1
full text available

Development Of Equipment For The Experimental Measurement Of The Moments Of Inertia, And Product Of Inertia Of Aircraft

Author(s): Claude R. Woodward
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1954-06
Report Number: WADC TR 54-237
full text available

Effects Of Structural Flexibility On Gust Loading Of Aircraft Part II: Dynamic Stresses In Swept-wing Airplanes

Author(s): A. A. Kirsch, J. M. Calligeros, K. A. Foss
Corporate Author: Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-08
Report Number: WADC TR 54-592 Part 2
full text available

Effects Of Structural Flexibility On Gust Loading Of Aircraft Part I: Gust Loads On Swept-wing Airplanes Free To Pitch And To Deform Statically

Author(s): K. A. Foss
Corporate Author: Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report Number: WADC TR 54-592 Part 1
full text available

The Effects Of Thermal Radiation On Aircraft Structures, Part I. The M.I.T. Mark I Radiant Heating Structural Test Facility

Author(s): John C. Loria; William J. Blackstock; James W. Mar
Corporate Author: Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1954-10
Report Number: WADC TR 54-384 Part 1
full text available

Analytical Studies Of Aircraft Structures Exposd To Transient External Heating Volume I Thermal Response Of A "Thin" Plate Under Influence Of A Constant Temperature Edge

Author(s): Alphonso Ambrosio; Takao Ishimoto
Corporate Author: University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Report Number: WADC TR 54-579 Volume 1
full text available

Analytical Studies Of Aircraft Structures Exposed To Transient External Heating. Vol. II: Thermal Response Of A Finite Plate And The "thin" Plate Criterion

Author(s): Alphonso Ambrosio, Takao Ishimoto
Corporate Author: University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1954-11
Report Number: WADC TR 54-579 Volume 2
full text available

The Effect of an Axially Symmetric Fuselage on the Nonstationary Supersonic Airloads Acting on a Wing with Supersonic Edges

Author(s): Melvin Epstein
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-05
Report Number: WADC TR 54-196
full text available

New Standard Atmosphere: The WADC 1952 Model Atmosphere

Author(s): D. T. Williams, J. C. Bell, W. F. Nash
Corporate Author: Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report Number: WADC TR 54-215
full text available

Theoretical Investigation Of Optimum Pressures In Aircraft Hydraulic Systems

Author(s): Conrad H. Cooke, Eugene Gessner, Robert L. Smith, Glenn L. Martin
Corporate Author: Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1954-01
Report Number: WADC TR 54-189 Volume 2
full text available