Call Number (LC) | Title | Results |
---|---|---|
NAS 1.60:2026 |
Establishment of a rotor model basis / Establishment of a rotor model basis |
2 |
NAS 1.60:2027 | Multiroller traction drive speed reducer : evaluation for automotive gas turbine engine / | 1 |
NAS 1.60:2028 | Venturi nozzle effects on fuel drop size and nitrogen oxide emissions / | 1 |
NAS 1.60:2029 | Velocity gradient method for calculating velocities in an axisymmetric annular duct / | 1 |
NAS 1.60:2030 | Computer program for calculating full potential transonic, quasi-three-dimensional flow through a rotating turbomachinery blade row / | 1 |
NAS 1.60:2031 | Calculation of composition distribution of ultrafine ion-H₂O-H₂SO₄ / | 1 |
NAS 1.60:2032 | Buckling test of a 3-meter-diameter corrugated graphite-epoxy ring-stiffened cylinder / | 1 |
NAS 1.60:2033 | The application of parameter estimation to flight measurements to obtain lateral-directional stability derivatives of an augmented jet-flap STOL airplane / | 1 |
NAS 1.60:2034 | Performance of a tandem-rotor/tandem-stator conical-flow compressor designed for a pressure ratio of 3 / | 1 |
NAS 1.60:2035 | Development and evaluation of a Kalman-filter algorithm for terminal area navigation using sensors of moderate accuracy / | 1 |
NAS 1.60:2036 | Plastic deformation at surface during unlubricated sliding / | 1 |
NAS 1.60:2037 | Wear mechanism based on adhesion. | 1 |
NAS 1.60:2038 | Studies of implicit and explicit solution techniques in transient thermal analysis of structures / | 1 |
NAS 1.60:2039 | Simplified free-energy calculation for ion-induced heteromolecular nucleation / | 1 |
NAS 1.60:2040 | Influence of corrosive solutions on microhardness and chemistry of magnesium oxide [001] surfaces / | 1 |
NAS 1.60:2042 | Experimental investigation of active loads control for aircraft landing gear / | 1 |
NAS 1.60:2043 | Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers / | 1 |
NAS 1.60:2044 | Aeropulsive characteristics at Mach numbers up to 2.2 of axisymmetric and nonaxisymmetric nozzles installed on an F-18 model / | 1 |
NAS 1.60:2045 | A stability analysis of AVE-IV severe weather soundings / | 1 |
NAS 1.60:2046 | Noise transmission loss of aircraft panels using acoustic intensity methods / | 1 |