000			01646 a2200109 4500
100			_aSmith, John W.
245	1		_aAnalysis of longitudinal pilot induced oscillation tendencies of yl-12 aircraft _cJohn W. Smith and Donald T. Berry
260			_aWashington _bNasa _c1975
440			_anational aeronautics and space administration
500			_aTR2631: Dyngen- a program for calculating steady and transient performance of turbojet and turbofan engines by James F. Sellers Report no. NASA TN D-7901 [1975] TR2632: Effect of number of lobes and length-diameter ratio on stability of tilted -lobe hydrodynamic journal bearings at zero load by Fredrick T. Schuller Report no. NASA TN D-7902 [1975] TR2633: A Photometric function for diffuse reflection by particulate materials by Willard E. Meador Report no. NASA TN D-7903 [1975] TR2634: Reproducibility of liquid oxygen impact test results by J.B. Gayle Report no. NASA TN D-7905 [1975] TR2635: Performance of an isolated two-dimensional variable-geometry wedge nozzle with translating shroud and collapsing wedge at speeds up to mach 2.01 by DDonald L. Maiden Report no. NASA TN D-7906 [1975] TR2636: Radiated noise from an externally blown flap by N.N. Reddy Report no. NASA TN D-7908 [1975] TR2637: Materials technology for an advanced space power nuclear reactor concept -program summary by Richard E. Gluyas Report no. NASA TN D-7909 [1975] TR2638: Effect of wing planform and canard location and geometry on the longitudinal aerodynamic characteristics of a close-coupled canard wing model at subsonic speeds by Blair B. Gloss Report no. NASA TN D-7910 [1975]
942			_cTR
999			_c391924 _d391924