Flight Load Measurements and Analysis Lockheed Aircraft Corporation

Format:

Conference/Event

Author/Creator:

Howland, W. L., author.

Conference Name:

SAE National Aeronautic Meeting

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1955

Summary:

KNOWLEDGE of loads on major structural parts of an airplane while in flight is needed for complete utilization of the airplane's strength and capabilities. Some in-flight measuring techniques and equipment for reducing the data thus obtained are discussed in this paper.Instrumentation and calibration of strain gages for measuring in-flight air loads are described in detail. Wing bending-moment measurements obtained on a Navy PV-2 airplane are used to illustrate data reduction procedure

Notes:

Vendor supplied data

Publisher Number:

550268

Access Restriction:

Restricted for use by site license