Error Due to Wing Bending in Single-Camera Photogrammetric Technique

By National Aeronautics and Space Administration

The error due to wing bending introduced into single-camera photogrammetric computations used for the determination of wing twist or control surface angular deformation is described. It is shown that the error due to wing bending when determining main wing element-induced twist is typically less than 0.05deg at the wing tip and may not warrant additional correction. It is also shown that the angular error in control surface deformation due to bending can be as large as 1deg or more if the control surface is at a large deflection angle compared to the main wing element. A correction procedure suitable for control surface measurements is presented. Simulations of the error based on typical wind tunnel measurement geometry, and results from a controlled experimental test in the test section of the National Transonic Facility (NTF) are presented to confirm the validity of the method used for correction of control surface photogrammetric deformation data. An example of a leading edge (LE) slat measurement is presented to illustrate the error due to wing bending and its correction. Burner, Alpheus W., Jr. and Barrows, Danny A. Langley Research Center NASA/TM-2005-213254, L-19021 WU 23-090-80-40 PHOTOGRAMMETRY; CONTROL SURFACES; DEFORMATION; WINGS; LEADING EDGES; WIND TUNNEL TESTS; CORRECTION; TEST CHAMBERS

• Format: Paperback
• Language: English
• ISBN: B08F6RYFM4
• ISBN13: 9798672454184
• Release Date: January 1
• Publisher: Independently Published
• Length: 32 Pages
• Weight: 0.22 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"