Call Number (LC) Title Results
NAS 1.60:1686 Computerized video densitometry method for rapid analysis of infrared photographic images / 1
NAS 1.60:1687 Dynamic behavior of a beam drag-force anemometer / 1
NAS 1.60:1688 Cold-air investigation of 4 1/2-stage turbine with stage-loading factor of 4.66 and high specific work output : II - stage group performance / 1
NAS 1.60:1689 Control-system techniques for improved departure/spin resistance for fighter aircraft / 1
NAS 1.60:1690 Programmer's manual for MMLE3, a general FORTRAN program for maximum likelihood parameter estimation / 1
NAS 1.60:1691 Long-time creep behavior of the tantalum alloy Astar 811C 1
NAS 1.60:1692 Static and transient performance of YF-102 engine with up to 14 percent core airbleed for the quiet short-haul research aircraft / 1
NAS 1.60:1693 Off-design correlation for losses due to part-span dampers on transonic rotors / 1
NAS 1.60:1694 Coordinated aircraft and ship surveys for determining impact of river inputs on Great Lakes Waters : remote sensing results / 1
NAS 1.60: 1696 Large-scale wind-tunnel tests of inverting flaps on a STOL utility aircraft model / 1
NAS 1.60:1697 Experimental investigation of the radiation of sound from an unflanged duct and a bellmouth, including the flow effect / 1
NAS 1.60:1698 Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue
Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue / 		2
NAS 1.60:1699 Crash tests of four identical high-wing single-engine airplanes / 1
NAS 1.60:1700 Development of the reentry flight dynamics simulator for evaluation of Space Shuttle Orbiter entry systems /
Development of the reentry flight dynamics simulator for evaluation of space shuttle orbiter entry systems 		2
NAS 1.60:1701 Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 /
Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 		2
NAS 1.60:1702 Release mechanism for releasing and reattaching experiments on the space shuttle / 1
NAS 1.60:1703 Aerothermal analysis of a wing-elevon cove with variable leakage /
Aerothermal analysis of a wing-elevon cove with variable leakage 		2
NAS 1.60:1704 The effect of throat contouring on two-dimensional converging-diverging nozzles at static conditions / 1
NAS 1.60:1705 CAS2D - FORTRAN program for nonrotating blade-to-blade, steady potential transonic cascade flows / 1
NAS 1.60:1706 Annoyance due to multiple airplane noise exposure / 1