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ESTIMATION OF STATIC LONGITUDINAL STABILITY OF AIRCRAFT CONFIGURATIONS AT HIGH MACH NUMBERS AND AT ANGLES OF ATTACK BETWEEN 0(DEGREE) AND +-180(DEGREE)

By: Dugan,Duane W.
Material type: materialTypeLabelBookPublisher: Nasa, Washington, D.C. 1962Description: 72.DDC classification: NASA | MEMO 1-17-59A -
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Item type Current location Collection Call number Status Date due Barcode Item holds
Technical Report Technical Report PK Kelkar Library, IIT Kanpur
General Stacks NASA MEMO 1-17-59A - (Browse shelf) Not for loan TR7771
Total holds: 0

Bound With Nasa Memo 1-8-59a-1-29-59a

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