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Ray H. Wright

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Books

Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4
Investigation of the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers from 1.24 to 7.4
United States. National Advisory Committee for Aeronautics, Franklyn B. Fuller, Edmund E. Callaghan, Willard D. Coles, Ray H. Wright, C. H. Wilts, Edward W. Perkins, Isadore L. Drell, Lewis Laboratory Staff, Max. A. Heaslet, Frank E. Belles, Leland H. Jorgensen, Virgil S. Ritchie, Albin O. Pearson, Simon C. Sommer
Test Sections for Small Theoretical Wind-tunnel-boundary Interference on V/STOL Models
Test Sections for Small Theoretical Wind-tunnel-boundary Interference on V/STOL Models
Ray H. Wright
Wind-tunnel Lift Interference on Sweptback Wings in Rectangular Test Sections with Slotted Top and Bottom Walls
Wind-tunnel Lift Interference on Sweptback Wings in Rectangular Test Sections with Slotted Top and Bottom Walls
Raymond L. Barger, Ray H. Wright

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