Drag Evaluation of the Bellanca Skyrocket II 770472
The Bellanca Skyrocket II, possessor of five world speed records, is a single engine aircraft with high performance that has been attributed to a laminar flow airfoil and an all composite structure. Utilization of composite materials in the Skyrocket II is unique since this selection was made to increase the aerodynamic efficiency of the aircraft. Flight tests are in progress to measure the overall aircraft drag and the wing section drag for comparison with the predicted performance of the Skyrocket. Initial results show the zero lift drag is indeed low, with CDO = 0.016.
Citation: Gregorek, G., Hoffmann, M., Payne, H., and Harris, J., "Drag Evaluation of the Bellanca Skyrocket II," SAE Technical Paper 770472, 1977, https://doi.org/10.4271/770472. Download Citation
Author(s):
G. M. Gregorek, M. J. Hoffmann, H. Payne, J. P. Harris
Affiliated:
The Ohio State University, Bellanca Aircraft Engineering
Pages: 16
Event:
National Business Aircraft Meeting and Engineering Display
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Aircraft
Composite materials
Drag
Flight tests
Aerodynamics
Wings
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