Call Number (LC) Title Results
NAS 1.15:86719 An evaluation of three helicopter rotor sections 1
NAS 1.15:86720 Star formation in the inner galaxy a far-infrared and radio study of two HII regions / 1
NAS 1.15:86721 Far-infrared emission lines of CO and OH in the Orion-KL molecular shock 1
NAS 1.15:86722 Observations of far-infrared transitions between excited states of OH 1
NAS 1.15:86723 Submillimeter observations of OH and CH in M42 1
NAS 1.15:86724 A numerical simulation of the NFAC (National Full-Scale Aerodynamics Complex) open-return wind tunnel inlet flow 1
NAS 1.15:86725 HiMAT flight program test results and program assessment overview / 1
NAS 1.15:86726 Digital program for calculating static pressure position error 1
NAS 1.15:86727 Formulation and implementation of nonstationary adaptive estimation algorithm with applications to air-data reconstruction 1
NAS 1.15:86728 Application of frequency domain handling qualities criteria to the longitudinal landing task 1
NAS 1.15:86729 A comparison of measured and calculated thermal stresses in a hybrid metal matrix composite spar cap element 1
NAS 1.15:86730 Extraction of aerodynamic parameters for aircraft at extreme flight conditions 1
NAS 1.15:86731 Qualification needs for advanced integrated aircraft 1
NAS 1.15:86732 Development of a temperature-compensated hot-film anemometer system for boundary-layer transition detection of high performance aircraft 1
NAS 1.15:86733 A Constant altitude flight survey method for mapping atmospheric ambient pressures and systematic radar errors 1
NAS 1.15:86735 Fault detection and accommodation testing on an F100 engine in an F-15 airplane 1
NAS 1.15:86736 Development of control laws for a flight test maneuver autopilot for an F-15 aircraft 1
NAS 1.15:86737 Development and validation of a general purpose linearization program for rigid aircraft models 1
NAS 1.15:86738 Flight test experience and controlled impact of a large, four-engine, remotely piloted airplane 1
NAS 1.15:86739 Design of an expert-system flight status monitor 1