Investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30(degree) sweptback wing at transonic speeds
By: Charles F Whitcomb.
Contributor(s): Philippa F Brown.
Material type:
BookPublisher: DDC classification: NASA | TN D-620 -
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA TN D-620 - (Browse shelf) | Not for loan | TR10235 |
Total holds: 0
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