Hinge Moments of Sealed-internal-balance Arrangements for Control Surfaces

Hinge Moments of Sealed-internal-balance Arrangements for Control Surfaces

Author: Harry E. Murray

Publisher:

Published: 1945

Total Pages: 46

ISBN-13:

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Summary: The results of a theoretical analysis of the hinge-moment characteristics of various sealed-internal-balance arrangement for control surfaces are presented. The analysis considered overhangs sealed to various types of wing structure by flexible seals spanning gaps of various widths or sealed to the wing structure by a flexible system of linked plates. Leakage was not considered; the seal was assumed to extend the full spanwise length of the control surface. The effect of the developed width of the flexible seal and of the geometry of the structure to which the seal was anchored was investigated, as well as the effect of the gap width that is sealed.


Hinge Moments of Sealed-internal-balance Arrangements for Control Surfaces

Hinge Moments of Sealed-internal-balance Arrangements for Control Surfaces

Author: Jack Fischel

Publisher:

Published: 1945

Total Pages: 66

ISBN-13:

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Summary: Tests were made in a seal test chamber to determine the hinge moments contributed by the fabric seal in an internal-balance arrangement employing a thin-plate over-hang. These tests were performed with various widths of fabric sealing various widths of flap-nose gap, with a horizontal, a vertical, and a circular type of wing structure forward of the balance, and with various heights of balance chamber. This investigation is an experimental verification and extension of a previous analytical investigation. The present investigation indicated that the moment of the seal may be a balancing or an unbalancing moment and may be an appreciable part of the total balancing moment of an internally balanced flap, depending on the overhang deflection and the configuration of the internal balance. Variation of the width of the fabric seal, the sealed gap, or the location of the seal attachment to the wing structure affected the seal moments through most of the over-hang deflection range. The shape and size of the balance chamber affected the seal-moment characteristics in the deflection range where the seals contacted and were constrained by the chamber walls; the values of the seal moments were usually reduced when the seals were constrained. The results indicated also that an optimum balance configuration would employ a seal width such that the seal would barely touch the chamber ceiling when maximum overhang deflection is attained.


Wartime Report

Wartime Report

Author:

Publisher:

Published: 194?

Total Pages: 762

ISBN-13:

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Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.


Wartime Report

Wartime Report

Author: United States. National Advisory Committee for Aeronautics

Publisher:

Published:

Total Pages: 288

ISBN-13:

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Flight Investigation of the Cooling Characteristics of a Two-row Radial Engine Installation

Flight Investigation of the Cooling Characteristics of a Two-row Radial Engine Installation

Author: E. Barton Bell

Publisher:

Published: 1946

Total Pages: 558

ISBN-13:

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Flight tests have been conducted to determine the cooling characteristics of a two-row radial engine at altitude in a twin-engine airplane and to investigate the accuracy with which low-altitude cooling-correlation equations can be used for making cooling predictions at higher altitudes. The test engine was operated over a wide range of condtions in level flight at density altitudes of 5000 and 20,000 feet.