Spreiter, J.R.
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Technical report. R–88 : Theoretical pressure distributions on wings of finite span at zero incidence for mach numbers near 1
1961
2635
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Technical notes. №2273 : Similarity laws for transonic flow about wings of finite span
1951
2432
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Technical report. 2 : Slender-body theory based on approximate solution of the transonic flow equation
1959
598
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Report. №1217 : Theoretical prediction of pressure distributions on nonlifting airfoils at high subsonic speeds
1955
1150
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Report. №1359 : Thin airfoil theory based on approximate solution of the transonic flow equation
1958
2503
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Technical report. R–177 : The effect of a ring current on the boundary of the geomagnetic field in a steady solar wind
1963
1883
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Technical report. 73 : A study of the simulation of flow with free-stream mach number 1 in a choked wind tunnel
1960
2940
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