Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system
Material type:
TextLanguage: English Publication details: Washington, D. C. National Advisory Committee for Aeronautics 1953Description: 41pDDC classification: - NACA TN-2882
| Item type | Current library | Collection | Call number | Status | Date due | Barcode | Item holds | |
|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | Reference | NACA TN-2882 (Browse shelf(Opens below)) | Not for loan | 67708B |
Total holds: 0
There are no comments on this title.
Log in to your account to post a comment.