Call Number (LC) Title Results
NAS 1.26:3053/v.1 Aerodynamic characteristics of forebody and nose strakes based on F-16 wind tunnel test experience ; prepared for Langley Research Center under contract NAS1-15006. 1
NAS 1.26:3054 Methods of separation of variables in turbulence theory / 1
NAS 1.26:3056 The free jet as a simulator of forward velocity effects on jet noise / 1
NAS 1.26:3057 The development of a three-dimensional partially elliptic flow computer program for combustor research / 1
NAS 1.26:3058 Experimental investigation of the subwing tip and its vortex structure / 1
NAS 1.26:3059 A comparative study of Conroy and Monte Carlo methods applied to multiple quadratures and multiple scattering / 1
NAS 1.26:3060 Helicopter mission optimization study / 1
NAS 1.26:3061 Investigation of steady and fluctuating pressures associated with the transonic buffeting and wing rock of a one-seventh scale model of the F-5A aircraft / 1
NAS 1.26:3063 A new blade element method for calculating the performance of high and intermediate solidity axial flow fans / 1
NAS 1.26:3064 Operational manual for two-dimensional transonic code TSFOIL / 1
NAS 1.26:3065 Analysis of a theoretically optimized transonic airfoil / 1
NAS 1.26:3066 The flying hot wire and related instrumentation / 1
NAS 1.26:3067 Study of mean-and turbulent velocity fields in a large-scale turbine-vane passage / 1
NAS 1.26:3068 Acoustic scattering by circular cylinders of various aspect ratios / 1
NAS 1.26:3069 Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations / 1
NAS 1.26:3070 Numerical computation of transonic flows by finite-element and finite-difference methods / 1
NAS 1.26:3071 Prediction of compliant wall drag reduction, part II / 1
NAS 1.26:3072 Prediction and monitoring of clear air turbulence : an evaluation of the applicability of the Rawinsonde system / 1
NAS 1.26:3073 Investigation of aircraft landing in variable wind fields / 1
NAS 1.26:3074 Development of a digital guidance and control law for steep approach automatic landings using modern control techniques / 1