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1. FORMULAS PERTINENT TO THE CALCULATION OF FLOW-FIELD EFFECTS AT SUPERSONIC SPEEDS DUE TO WING THICKNESS

by Margolis,Kenneth | Elliott,Miriam H.

Material type: book Book Description: 26.Publisher: Nasa, Washington, D.C. 1959Availability: No items available Damaged (1).

2. NASA Technical Note [NASA TN D-383]: Theoretical calculations of the pressures forces, and moments due to various lateral motions acting on tapered sweptback vertical tails with supersonic leading and trailing edges

by Washington. National Aeronautics and Space Administration (NASA) | Margolis, Kenneth | Elliott, Miriam H.

Material type: book Book Description: 126p.Publisher: Washington NASA 1960Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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