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Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
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Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 : Reports 337-364 [texte imprimé] / National advisory committee for aeronautics, Auteur . - Washington : Government printing office, 1931 . - 787p. : ill. noir&blanc ; 30 x 24 cm + schémas, plans, tableaux. - (National Advisory Committee for Aeronautics; N°337-364) . Langues : Anglais (eng)
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- The Gaseous Explosive Reaction at Constant Pressure - The Reaction Order ans Reaction Rate - Report N°337 / F. W. STEVENS
- Large-Scale Aerodynamic Characteristics of Airfoils as Tested in the Variable Density Wind Tunnel - Report N°352 / Eastman N. JACOBS
- Airfoil Pressure Distribution Investigation in the Variable Density Wind Tunnel - Report N°353 / Eastman N. JACOBS
- Aircraft Woods : Their Properties, Selection, and Characteristics - Report N°354 / L. J. MARKWARDT
- Comparative Flight Performance with an NACA Roots Supercharger and a Turbocentrifugal Supercharger - Report N°355 / Oscar W. SCHEY
- Strength of Rectangular Flat Plates Under Edge Compression - Report N°356 / Louis SCHUMAN
- Aircraft Accidents-Method of Analysis - Report N°357 / Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics
- Temparature Coefficient of the Modulus of Rigidity of Aircraft Instrument Diaphragm and Spring Materials - Report N°358 / W. G. BROMBACHER
- An Investigation of the Effectiveness of Ignition Sparks - Report N°359 / Melville F. PETERS
- Pressure Distribution over a Symmetrical Airfoil Section with Trailing Edge Flap - Report N°360 / Eastman N. JACOBS
- Experimental Determination of Jet Boundary Corrections for Airfoil Test in Four Open Wind Tunnel Jets of Different Shapes - Report N°361 / Montgomery KNIGHT
- An Extended Theory of Thin Airfoils and its Application to the Biplane Problem - Report N°362 / Clark B. MILLIKAN
- Pressure Fluctuations in a Common-Rail Fuel Injection System - Report N°363 / A. M. ROTHROCK
- Full Scale Wind Tunnel Test of a Propeller with the Diameter Changed by Cutting Off the Blade Tips - Report N°351 / Donald H. WOOD
- Working Charts for the Selection of Aluminum Alloy Propellers of a Standard Form to Operate with Varius Aircraft Engines and Bodies - Report N°350 / Fred E. WEICK
- The Effect of Reduction Gearing on propeller-Body Interference as Shown by Full Scale Wind Tunnel Test - Report N°338 / Fred E. WEICK
- Full Scale Wind Tunnel Test with a Series of Propellers of Different Diameters on a Single Fuselage - Report N°339 / Fred E. WEICK
- Full Scale Wind Tunnel Tests on Several Metal Propellers Having Different Blade Forms - Report N°340 / Fred E. WEICK
- The Design and Develpment of an Automatic Injection Valve with an Annular Orifice of Varying Area - Report N°341 / William F. JOACHIM
- Effect of Turbulence in Wind Tunnel Measurements - Report N°342 / H. L. DRYDEN
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