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An Experimental Investigation Of Hot Gas Ejectors For Boundary Layer Control
Author(s): De Leo, Richard V.Corporate Author(s): Rosemount Aeronautical Laboratories, University of Minnesota
Laboratory: Aircraft Laboratory
Date of Publication: 1953-12
Report number: WADC TR 52-128 Part 2
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Method For Predicting Dynamic Landing Loads
Author(s): Eisenman, Richard L., Kramer, Edward H.Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-09
Report number: WADC TR 54-28
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An Investigation Of The Experimental Determination Of Aircraft Inertia
Author(s): Woodard, Claude R.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-207
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Boundary Layer Control On 64A006 And 64A010 Airfoils At High Subsonic Speeds
Author(s): Leadon, B. M. , Anderson, G. E.Corporate Author(s): Dept. Of Aeronautical Engineering, University Of Minnesota
Laboratory: Aircraft Laboratory
Date of Publication: 1953-10
Report number: WADC TR 53-490
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The Wall Pressure Distribution In A Choked Tunnel
Author(s): Guderley, GottfriedCorporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1953-12
Report number: WADC TR 53-509
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Temperature Distributions In A Typical Aircraft Structure Due To Transient External Heating, Volume I, T-33 Airplane
Author(s): Ambrosio, Alphonso, Bussell, Bertram, Macinnes, William F.Corporate Author(s): University Of California, Department Of Engineering, Los Angeles, California
Laboratory: Aircraft Laboratory
Date of Publication: 1953-04
Report number: WADC TR 52-216
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Thermo-Elastic Stresses And Deflections In Beam-Columns
Author(s): Boley, Bruno A., Mechanic, HaroldCorporate Author(s): Institute Of Air Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-425
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Thermo-Elastic Stresses And Deflections In Thin-Walled Beams
Author(s): Boley, Bruno A., Tolins, Irwin S.Corporate Author(s): Institute Of Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-12
Report number: WADC TR 54-426
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Destruction Tests Of Aircraft Structural Components; Part 2. Development Of A Single-Channel Bending Moment Measurement Method Applicable To A Complex Built-Up Structure For Both The Elastic And The Post-Buckling Regime Of Structural Response
Author(s): Criscione, Emanuel S., Ayvazian, Mi Hran, Wetmore, Kenneth R.Corporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-09
Report number: WADC TR 54-385 Part 2
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A Method For The Approximate Solution Of The Heat Equation
Author(s): Weiner, Jerome H.Corporate Author(s): Institute Of Flight Structures,Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 54-427
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- Boley, Bruno A. (5)
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