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activities additional AERONAUTICS AND SPACE aeroshell analysis angle of attack Apollo atmospheric balance barium beam blowing buckling calculated cathode Center chamber changes chord coefficient complex composite considered container critical curve determine distribution dose effect electron element energy engine equation error estimates exposure filament flap deflection flow force fraction frequency fringe function given glove increase increment indicate initial lens less lift light limited load located material matrix mean measurements mode momentum coefficient NASA normal noted nozzle obtained occur operator particle percent Performing position presented pressure procedure processing radiation range ratio reference ring sample shown in figure shows signal Space spectral spectrum stress surface TECHNICAL temperature thickness tion transfer tungsten turbulence unit vacuum values volume
Page 34 - As an aid to the reader, where necessary the original units of measure have been converted to the equivalent value in the Systeme International d
Page 129 - G-1011 9. Performing Organization Name and Address 10. Work Unit No. Goddard Space Flight Center Greenbelt, Maryland 20771 11. Contract or Grant No. 12. Sponsoring Agency Name and Address 13.
Page 16 - US Customary Units. The measurements and calculations were made in US Customary Units.
Page 31 - AMES RESEARCH STAFF : Equations, Tables, and Charts for Compressible Flow. NACA Rep. 1135, 1953.
Page 13 - Effects of upper-surface blowing and thrust vectoring on low-speed aerodynamic characteristics of a large-scale supersonic transport model...
Page 31 - Carl J.. and Harris, Thomas A.: Wind-Tunnel Investigation of an NACA 23012 Airfoil with Various Arrangements of Slotted Flaps.