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