March 1971 wind tunnel tests of the Dorand DH 2011 jet flap motor, volume 2 [PDF]
Wind tunnel tests were conducted of the Dorand DH 2011D jet flap rotor. The data recorded during the tests consist of: (1) multicyclic cam coefficients, (2) stress analysis, (3) vibratory loads, (4) Fourier analysis of flap deflection, and (5) blade ...
Aubrun, J., Kretz, M., Larche, M.
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Reconstruction of extensive craniofacial defect following paraganglioma excision using a chimeric anterolateral thigh flap: a case report. [PDF]
Case Reports Plast Surg Hand SurgTuấn Nghĩa P, Nam ĐP, Sơn TT.
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How I do it: exoscopic minimally invasive pericranial flap harvest for endoscopic anterior skull base reconstruction. [PDF]
Acta Neurochir (Wien)Wiedmann MKH +3 more
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An experimental and theoretical investigation of thick wings at various sweep angles in and out of ground effect [PDF]
The effects of sweep and aspect ratio on the longitudinal aerodynamics of a wing in and out of ground effect are analyzed. Experimental data were obtained in the Langley 4 by 7 Meter Tunnel for a wing with various sweep angles, aspect ratios, and flap ...
Kjelgaard, S. O., Paulson, J. W., Jr.
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Versatile Three-Dimensional Head and Neck Reconstruction Using a Thoracodorsal Artery-Based Chimeric Flap: A Bi-Institutional Experience. [PDF]
J Clin MedKim YH, Hong SE, Kang D.
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The "Pacman Flap with Tongue" for Secondary Orbital Reconstruction in Osteoradionecrosis: A Case Series. [PDF]
Medicina (Kaunas)Gontarz M +6 more
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An experimental study of pressures on 60 deg Delta wings with leading edge vortex flaps [PDF]
An experimental study was conducted in the Virginia Tech Stability Wind Tunnel to determine surface pressures over a 60 deg sweep delta wing with three vortex flap designs.
Donatelli, D. A. +2 more
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Reconstruction of combined bone and soft tissue defects of the hand and foot with free superficial circumflex iliac artery perforator osteocutaneous flaps: a retrospective analysis. [PDF]
Front SurgPan J +5 more
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Calculation of static longitudinal aerodynamic characteristics of STOL aircraft with upper surface blown flaps [PDF]
An existing prediction method developed for EBF aircraft configurations was applied to USB configurations to determine its potential utility in predicting USB aerodynamic characteristics. An existing wing-flap vortex-lattice computer program was modified
Goodwin, F. K. +3 more
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