NASA TM [X-92] : EFFECTS OF WING-CRANK, LEADING-EDGE EXTENSIONS AND HORIZONTAL-TALL HEIGHT ON THE LONGITUDINAL STABILITY OF SWEPT-WING MODELS AT MACH NUMBERS FROM 0.6 TO 1.4
By: Wakefield, Roy M.
Series: NASA Technical Memorandum. Publisher: Nasa, Washington, D.C. 1959Description: 116.Subject(s): Aerodynamics| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | General Stacks | NASA TM X-92 - (Browse shelf) | Not for loan | TR9395 |
Total holds: 0
NASA Technical Memorandum X-71;72;75;83;85;86;89;92;100
Bounded Volumes Accession No. 102471; Contents: TR9389-96
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