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Preliminary wing model tests in the variable density wind tunnel of the National Advisory Committee for Aeronautics (1926)
NASA Technical Reports Server (NTRS) · leaf 6
209 PRELIMINARY WING MODEL TESTS … 1.4 l£ 1.0 08 Q.6 i 0.4 aa ao .OO .04 .08 J2 JG £0 £4 £8 ao -oj -as -0.3 -0.4 -as -0.6 -a? Gtfqbout quarter chord} Fli> U—Test No. 58-3. Tank pressure 8 atmospheres. Dynamic pressure Fig. 12.—Test No. 58-t. Tank pressure 18 atmospheres. Dynamic pressure j-248kg/m». Reynolds Number 1,430,000 j—524…NASA Technical Reports Server (NTRS)
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