NASA Technical NoteNational Aeronautics and Space Administration., 1960 |
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Common terms and phrases
acceleration aerodynamic afterbody airplane altitude Aluminum amplitude angle of attack angle-of-attack angular aspect ratio azimuth angle burnout calculated characteristics coefficient compression configuration constant Copper Crater cylinder damping deceleration decrease deflection delta wing determined Diam diffuser earth earth-moon eccentricity effect elastic limit Enthalpy Entropy entry angle equation feet flight flow flutter frequency ft/sec function fuselage ground effect H/RTO half-span inch increased indicated induced velocity investigation Langley Field Langley Research Center latitude Lead lift Mach number measured miles missile moon motion NACA NASA nozzle oblateness obtained orbit oscillation oxidation penetration percent pilot pitch pitching moment pitching-moment plane position projectile range reference Reynolds number roll rotating rotor satellite shown in figure simulated sphere 22 stagnation stagnation pressure Steel supersonic surface swept spoiler target TECHNICAL NOTE temperature tests tion trailing-edge spoiler tunnel unswept values variation vehicle vorticity yield strength zero
Popular passages
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