Supplementary charts for estimating performance of high-performance helicopters
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Gessow, Alfred↗
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Charts for estimating rotor-blade flapping motion of high-performance helicopters
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Tapscott, Robert J↗
Experimental investigation of eccentricity ratio, friction, and oil flow of long and short journal bearings with load-number charts
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Dubois, G B↗
Charts of Boundary-layer Mass Flow and Momentum for Inlet Performance Analysis Mach Number Range, 0.2 to 5.0
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Simon, Paul C↗
Charts for the Analysis of Flow in a Whirling Duct
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Makofski, Robert A↗
Cascade Investigation of a Related Series of 6-percent-thick Guide-vane Profiles and Design Charts
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Dunavant, James C↗
Charts for Estimating the Effects of Short-period Stability Characteristics on Airplane Vertical-acceleration and Pitch-angle Response in Continuous Atmospheric Turbulence
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Pratt, Kermit G↗
Charts relating the compressive and shear buckling stresses of longitudinally supported plates to the effective deflectional stiffness
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Johnson, Aldie E↗
Charts for estimation of the profile drag-lift ratio of a helicopter rotor having rectangular blades with -8 degree twist
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Gustafson, F B↗
Charts giving critical compressive stress of continuous flat sheet divided into parallelogram-shaped panels
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Anderson, Roger A↗
Charts of thermodynamic properties of fluids encountered in calculations of internal combustion engine cycles
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Hottel, H C↗
Analysis and Construction of Design Charts for Turbines with Downstream Stators
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Cavicchi, Richard H↗
Cascade investigation of a related series of 6-percent-thick guide-vane profiles and design charts
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Dunavant, James C↗
Tables and Charts for Thermodynamic Calculations Involving Air and Fuels Containing Boron, Carbon, Hydrogen, and Oxygen
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Hall, Eldon W↗
Representative operating charts of propellers tested in the NACA 20-foot propeller-research tunnel
Report presents the results of tests of full-scale propellers made in the 20-foot propeller-research tunnel (PRT) at the Langley Memorial Aeronautical Laboratory. The power coefficients of all dual-rotating propellers in the report represent the sum of the power coefficients of the front and rear propellers and are for the test conditions in which blade angles of the front and rear propellers were set to absorb approximately equal power at peak efficiency only.
Gray, W H↗
Charts of Pressure, Density, and Temperature Changes at an Abrupt Increase in Cross-sectional Area of Flow of Compressible Air
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Joyner, Upshur T↗
Derivation of charts for determining the horizontal tail load variation with any elevator motion
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Pearson, Henry A↗
Generalized Selection Charts for Bombers Powered by Two, Four, and Six 3000-horsepower Engines I : Capacity and Economy
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Hill, Paul R↗