EFFECTS OF FOREBODY DEFLECTION ON STABILITY AND CONTROL CHARACTERISTICS OF A CANARD AIRPLANE CONFIGURATION WITH A HIGH TRAPEZOIDAL WING AT A MACH NUMBER OF 2.01
By: Spearman,M Leroy.
Contributor(s): Driver,Cornelius.
Material type:
BookPublisher: Nasa, Washington, D.C. 1959Description: 28.DDC classification: NASA | MEMO 4-4-59L -
| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA MEMO 4-4-59L - (Browse shelf) | Not for loan Untraceable | TR7689 |
Total holds: 0
Bound With Nasa Memo 4-1-59l-4-19-59l
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