Call Number (LC) Title Results
NAS 1.26:2737 The effect of helicopter main rotor blade phasing and spacing on performance, blade loads, and acoustics / 1
NAS 1.26:2738 The effect of configuration on strength, durability, and handle of Kevlar fabric-based materials / 1
NAS 1.26:2739 Development and field testing of a light aircraft oil surveillance system (LAOSS) / 1
NAS 1.26:2740 Effect of inlet temperature and pressure on emissions from a premixing gas turbine primary zone combustor / 1
NAS 1.26:2741 Analysis of the effect of numbers of aircraft operations on community annoyance / 1
NAS 1.26:2742 STAN5 - a program for numerical computation of two-dimensional internal and external boundary layer flows / 1
NAS 1.26:2743 Study of metallic structural design concepts for an arrow wing supersonic cruise configuration / 1
NAS 1.26:2745 Investigation of the effects of nonhomogeneous (or nonstationary) behavior on the spectra of atmospheric turbulence / 1
NAS 1.26:2746 User evaluation of ride technology research / 1
NAS 1.26:2747 Transonic performance of a Mach 2.65 auxiliary flow axisymmetric inlet / 1
NAS 1.26:2748 The inviscid pressure field on the tip of a semi-infinite wing and its application to the formation of a tip vortex / 1
NAS 1.26:2749 Turbulent atmospheric flow over a backward-facing step / 1
NAS 1.26:2750 Atmospheric flow over two-dimensional bluff surface obstructions / 1
NAS 1.26:2751 Estimates of the low-level wind shear and turbulence in the vicinity of Kennedy International Airport on June 24, 1975 / 1
NAS 1.26:2752 Wind shear and turbulence around airports / 1
NAS 1.26:2753 Studies of earth simulation experiments. 1
NAS 1.26:2754 Real-time testing of titanium sheet and extrusion coupon specimens subjected to Mach 2.7 supersonic cruise aircraft wing stresses and temperatures / 1
NAS 1.26:2755 Electrophoretic characterization of aldehyde-fixed red blood cells, kidney cells, lymphocytes and chamber coatings / 1
NAS 1.26:2756 Products of the reaction of chlorine atoms and ozone / 1
NAS 1.26:2757 A comparison between Nimbus 5 THIR and ITPR temperatures and derived winds with rawinsonde data obtained in the AVE II experiment / 1