Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method /
L.W. Mohn.

APA Citation

Mohn, L. Wayne., Langley Research Center., Boeing Commercial Airplane Company. (1975). Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method. Washington, D.C.: National Aeronautics and Space Administration .

MLA Citation

Mohn, Larry Wayne, Langley Research Center, and Boeing Commercial Airplane Company. Comparison of Wind-tunnel Test Results At M[subscript Infinity] = 0.7 With Results From the Boeing TEA-230 Subsonic Flow Method. Washington, D.C.: National Aeronautics and Space Administration , 1975.