Call Number (LC) Title Results
NAS 1.14:D-7179 Computer program for structural analysis of layered orthotropic rings-stiffened shells of revolution (SALORS) : linear stress analysis option / 1
NAS 1.14:D-7180 An analysis of a charring ablator with thermal nonequilibrium, chemical kinetics, and mass transfer / 1
NAS 1.14:D-7181 Thermodynamic and transport properties of gaseous tetrafluoromethane in chemical equilibrium / 1
NAS 1.14:D-7182 Description and calibration of the Langley 6- by 19-inch transonic tunnel / 1
NAS 1.14:D-7184 A multispectral study of an extratropical cyclone with Nimbus 3 medium resolution infrared radiometer data / 1
NAS 1.14:D-7185 Theoretical and experimental internal flow characteristics of a 13.97-centimeter-diameter inlet at STOL takeoff and approach conditions / 1
NAS 1.14:D-7186 Aluminum runway surface as possible aid to aircraft braking / 1
NAS 1.14:D-7187 Performance of an ion-cyclotron-wave plasma apparatus operated in the radiofrequency-sustained mode / 1
NAS 1.14:D-7188 Analytical and experimental performance of optimal controller designs for a supersonic inlet / 1
NAS 1.14:D-7189 Chemical nonequilibrium effects on the inviscid flow in the windward plane of symmetry of two simplified shuttle configurations / 1
NAS 1.14:D-7190 Evaluation of compressible-flow Preston tube calibrations / 1
NAS 1.14:D-7191 Aerodynamic characteristics of a vectored-thrust V/STOL fighter in the transition-speed range / 1
NAS 1.14:D-7192 Effect of fineness ratio on boattail drag of circular-arc afterbodies having closure ratios of 0.50 with jet exhaust at Mach numbers up to 1.30 / 1
NAS 1.14:D-7193 Application of phase-change technique to thin sections with heating on both surfaces / 1
NAS 1.14:D-7194 Wind-tunnel investigation of effects of variations in Reynolds number and leading-edge treatment on the aerodynamic characteristics of an externally blown jet-flap configuration / 1
NAS 1.14:D-7195 Calculation of energy deposition distributions for simple geometries / 1
NAS 1.14:D-7196 Comparison of the aerodynamic characteristics of an ablating and nonablating blunted conical body / 1
NAS 1.14:D-7197 A method for predicting shock shapes and pressure distributions on two-dimensional airfoils at large angles of attack / 1
NAS 1.14:D-7198 Experimental test results of a generalized-parameter fuel control / 1
NAS 1.14:D-7199 Aerodynamic effects of five lift-fan pod arrangements on an unpowered V/STOL transport model / 1