Drag Evaluation of the Bellanca Skyrocket II

770472

02/01/1977

Event
National Business Aircraft Meeting and Engineering Display
Authors Abstract
Content
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.
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DOI
https://doi.org/10.4271/770472
Pages
16
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.
Additional Details
Publisher
Published
Feb 1, 1977
Product Code
770472
Content Type
Technical Paper
Language
English