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NAS 1.60:1748
|
A modified T-value method for selection of strain gages for measuring loads on a low aspect ratio wing |
1 |
|
NAS 1.60:1750
|
Environmental analysis of the Chemical Release Module program |
1 |
|
NAS 1.60:1751
|
A new look at numerical analyses of free-edge stresses in composite laminates |
1 |
|
NAS 1.60:1752
|
A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel |
1 |
|
NAS 1.60:1753
|
Method for estimating crack-extension resistance curve from residual-strength data |
1 |
|
NAS 1.60:1754
|
Surface pyrometry in presence of radiation from other sources with application to turbine-blade temperature measurement |
1 |
|
NAS 1.60:1755
|
Effects of erodant particle shape and various heat treatments on erosion resistance of plain carbon steel |
1 |
|
NAS 1.60:1757
|
Modular instrumentation system for real-time measurements and control on reciprocating engines |
1 |
|
NAS 1.60:1758
|
Pseudosteady-state analysis of nonlinear aircraft maneuvers |
1 |
|
NAS 1.60:1760
|
Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stability |
1 |
|
NAS 1.60:1761
|
Mechanical property characterization of Borsic®/aluminum laminates at room and elevated temperatures |
1 |
|
NAS 1.60:1762
|
Use of constrained optimization in the conceptual design of a medium-range subsonic transport |
1 |
|
NAS 1.60:1763
|
Spatial frequency response of an optical heterodyne receiver |
1 |
|
NAS 1.60:1764
|
In-flight boundary-layer measurements on a hollow cylinder at a Mach number of 3.0 |
1 |
|
NAS 1.60:1766
|
Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft |
1 |
|
NAS 1.60:1767
|
Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 |
1 |
|
NAS 1.60:1770
|
Radio-wave propagation for space communications systems |
1 |
|
NAS 1.60:1771
|
Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles |
1 |
|
NAS 1.60:1775
|
Vibration characteristics of a steadily rotating slender ring |
1 |
|
NAS 1.60:1777
|
Leading-edge deflection optimization for a highly swept arrow-wing configuration |
1 |