Comparison of experimental and theoretical static aeroelastic loads and deflections of a thin 45 deg delta wing in supersonic flow [NASA TN D-974]
Material type:
TextLanguage: English Series: National Aeronautics and Spce Administratio (NASA)Publication details: Nasa, Washington, D.C. 1961Description: 41pSubject(s):
Contents:
Technical Note D-974
| Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds | |
|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | Not for loan | TR13289 [TN D-974] |
Total holds: 0
Bound With Nasa Tn D-971-973,975-980
Technical Note D-974
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