- Restrictions on Access:
- Unclassified, Unlimited, Publicly available.
- Pressure and spanwise load distributions on a first-generation jet transport semispan model at a Mach number of 0.30 are given for the basic wing and for configurations with an upper winglet only, upper and lower winglets, and a simple wing-tip extension. To simulate second-segment-climb lift conditions, leading- and/or trailing-edge flaps were added to some configurations.
- NASA Technical Reports Server (NTRS) Collection.
- Document ID: 19780012120.
Accession ID: 78N20063.
- No Copyright.
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