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1. An experimental investigation of interference between wings and body of three planar and cruciform rectangular wing and body combinations at mach numbers of 2.00 and 2.58

by E.R.A. Landers.

Material type: book Book Publisher: Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: TR ACA-68] (1).

2. Pressure distributions on planar and cruciform delta wing attached to cylindrical bodies in supersonic flow

by E.R.A. Landers.

Material type: book Book Publisher: Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: TR ACA-70] (1).

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