Calculation of the chordwise load distribution over airfoil sections with plain,split,or serially hinged traniling-edge flaps[R.No.634]
By: Allen,H.Julian.
Material type:
BookSeries: National Advisory Committee For Aeronautics(NACA). Publisher: Washington,D.C. National Advisory Committee For Aeronautics 1938Description: 16p.Subject(s): Calculation
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | Reference | 69740[R.No.634] |
Total holds: 0
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