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Analysis of flight-determined and predicted effects of flexibility on the steady-state wing loads of the B-52 airplane
From Introduction: "This paper presents the results obtained during the phase of the B-52 flight investigation concerned with the steady-state wing loads. Where possible, the effects of Mach number and flexibility on the measured load are analyzed and presented."
Date:
April 23, 1958
Creator:
Kuhl, Albert E.; Rogers, John T. & Little, Mary V.
System:
The UNT Digital Library
Analysis of Flight-Determined and Predicted Effects of Flexibility on the Steady-State Wing Loads of the B-52 Airplane
Memorandum presenting an investigation of the steady-state wing loads conducted on a Boeing B-52 airplane over a range of Mach numbers and altitudes. Results regarding flight tests and air-load calculations are provided.
Date:
April 23, 1958
Creator:
Kuhl, Albert E.; Rogers, John T. & Little, Mary V.
System:
The UNT Digital Library
Argonne National Laboratory Experimental and Theoretical Nuclear Physics Divisions Quarterly Report: January-March 1948
Quarterly report discussing the progress made with various projects at Argonne National Laboratory during the period from January to March 1948.
Date:
April 9, 1948
Creator:
Hughes, D. J. & Hoyt, Frank Clark
System:
The UNT Digital Library