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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
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) The Gaseous Explosive Reaction at Constant Pressure - The Reaction Order ans Reaction Rate - Report N°337 [texte imprimé] / F. W. STEVENS, Auteur . - [s.d.] . - P.67-83 : ill. noir&blanc, photo. Langues : Anglais (eng) |
Large-Scale Aerodynamic Characteristics of Airfoils as Tested in the Variable Density Wind Tunnel - Report N°352 / Eastman N. JACOBS
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Large-Scale Aerodynamic Characteristics of Airfoils as Tested in the Variable Density Wind Tunnel - Report N°352 [texte imprimé] / Eastman N. JACOBS, Auteur ; Raymon F. ANDERSON, Auteur . - [s.d.] . - p.419-450. Langues : Anglais (eng) |
Airfoil Pressure Distribution Investigation in the Variable Density Wind Tunnel - Report N°353 / Eastman N. JACOBS
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Airfoil Pressure Distribution Investigation in the Variable Density Wind Tunnel - Report N°353 [texte imprimé] / Eastman N. JACOBS, Auteur ; John H. STACK, Auteur ; Robert M. PINKERTON, Auteur . - [s.d.] . - p.451-466. Langues : Anglais (eng) |
Aircraft Woods : Their Properties, Selection, and Characteristics - Report N°354 / L. J. MARKWARDT
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Aircraft Woods : Their Properties, Selection, and Characteristics - Report N°354 [texte imprimé] / L. J. MARKWARDT, Auteur . - [s.d.] . - p.467-500. Langues : Anglais (eng) |
Comparative Flight Performance with an NACA Roots Supercharger and a Turbocentrifugal Supercharger - Report N°355 / Oscar W. SCHEY
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Comparative Flight Performance with an NACA Roots Supercharger and a Turbocentrifugal Supercharger - Report N°355 [texte imprimé] / Oscar W. SCHEY, Auteur ; Alfred W. YOUNG, Auteur . - [s.d.] . - p.501-514 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
Strength of Rectangular Flat Plates Under Edge Compression - Report N°356 / Louis SCHUMAN
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Strength of Rectangular Flat Plates Under Edge Compression - Report N°356 [texte imprimé] / Louis SCHUMAN, Auteur ; Goldie BLACK, Auteur . - [s.d.] . - p.515-538 : ill. noir&blanc, schémas. Langues : Anglais (eng) |
Aircraft Accidents-Method of Analysis - Report N°357 / Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Aircraft Accidents-Method of Analysis - Report N°357 [texte imprimé] / Committee on Aircraft Accidents of the National Advisory Committee for Aeronautics, Auteur . - [s.d.] . - p.539-555. Langues : Anglais (eng) |
Temparature Coefficient of the Modulus of Rigidity of Aircraft Instrument Diaphragm and Spring Materials - Report N°358 / W. G. BROMBACHER
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Temparature Coefficient of the Modulus of Rigidity of Aircraft Instrument Diaphragm and Spring Materials - Report N°358 [texte imprimé] / W. G. BROMBACHER, Auteur ; E. R. MELTON, Auteur . - [s.d.] . - p.557-572 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
An Investigation of the Effectiveness of Ignition Sparks - Report N°359 / Melville F. PETERS
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) An Investigation of the Effectiveness of Ignition Sparks - Report N°359 [texte imprimé] / Melville F. PETERS, Auteur ; Wayne L. SUMMERVILLE, Auteur . - [s.d.] . - p.573-585 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
Pressure Distribution over a Symmetrical Airfoil Section with Trailing Edge Flap - Report N°360 / Eastman N. JACOBS
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Pressure Distribution over a Symmetrical Airfoil Section with Trailing Edge Flap - Report N°360 [texte imprimé] / Eastman N. JACOBS, Auteur ; Robert M. PINKERTON, Auteur . - [s.d.] . - p.587-605 : ill. noir&blanc, schémas. Langues : Anglais (eng) |
Experimental Determination of Jet Boundary Corrections for Airfoil Test in Four Open Wind Tunnel Jets of Different Shapes - Report N°361 / Montgomery KNIGHT
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Experimental Determination of Jet Boundary Corrections for Airfoil Test in Four Open Wind Tunnel Jets of Different Shapes - Report N°361 [texte imprimé] / Montgomery KNIGHT, Auteur ; Thomas A. HARRIS, Auteur . - [s.d.] . - p.607-633 : ill. noir&blanc, photos, schémas. Langues : Anglais (eng) |
An Extended Theory of Thin Airfoils and its Application to the Biplane Problem - Report N°362 / Clark B. MILLIKAN
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) An Extended Theory of Thin Airfoils and its Application to the Biplane Problem - Report N°362 [texte imprimé] / Clark B. MILLIKAN, Auteur . - [s.d.] . - p.635-667 : ill. noir&blanc, schémas. Langues : Anglais (eng) |
Pressure Fluctuations in a Common-Rail Fuel Injection System - Report N°363 / A. M. ROTHROCK
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Pressure Fluctuations in a Common-Rail Fuel Injection System - Report N°363 [texte imprimé] / A. M. ROTHROCK, Auteur . - [s.d.] . - p.669-684 : ill. noir&blanc, schémas. Langues : Anglais (eng) |
Full Scale Wind Tunnel Test of a Propeller with the Diameter Changed by Cutting Off the Blade Tips - Report N°351 / Donald H. WOOD
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Full Scale Wind Tunnel Test of a Propeller with the Diameter Changed by Cutting Off the Blade Tips - Report N°351 [texte imprimé] / Donald H. WOOD, Auteur . - [s.d.] . - p.393-417 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
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
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Working Charts for the Selection of Aluminum Alloy Propellers of a Standard Form to Operate with Varius Aircraft Engines and Bodies - Report N°350 [texte imprimé] / Fred E. WEICK, Auteur . - [s.d.] . - p.377-392. Langues : Anglais (eng) |
The Effect of Reduction Gearing on propeller-Body Interference as Shown by Full Scale Wind Tunnel Test - Report N°338 / Fred E. WEICK
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) The Effect of Reduction Gearing on propeller-Body Interference as Shown by Full Scale Wind Tunnel Test - Report N°338 [texte imprimé] / Fred E. WEICK, Auteur . - [s.d.] . - P.85-105 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
Full Scale Wind Tunnel Test with a Series of Propellers of Different Diameters on a Single Fuselage - Report N°339 / Fred E. WEICK
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Full Scale Wind Tunnel Test with a Series of Propellers of Different Diameters on a Single Fuselage - Report N°339 [texte imprimé] / Fred E. WEICK, Auteur . - [s.d.] . - P.105-120 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
Full Scale Wind Tunnel Tests on Several Metal Propellers Having Different Blade Forms - Report N°340 / Fred E. WEICK
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Full Scale Wind Tunnel Tests on Several Metal Propellers Having Different Blade Forms - Report N°340 [texte imprimé] / Fred E. WEICK, Auteur . - [s.d.] . - P.121-133 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
The Design and Develpment of an Automatic Injection Valve with an Annular Orifice of Varying Area - Report N°341 / William F. JOACHIM
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) The Design and Develpment of an Automatic Injection Valve with an Annular Orifice of Varying Area - Report N°341 [texte imprimé] / William F. JOACHIM, Auteur ; Chester W. HICKS, Auteur . - [s.d.] . - P.135-144 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
Effect of Turbulence in Wind Tunnel Measurements - Report N°342 / H. L. DRYDEN
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Effect of Turbulence in Wind Tunnel Measurements - Report N°342 [texte imprimé] / H. L. DRYDEN, Auteur ; A. M. KUETHE, Auteur . - [s.d.] . - P.145-170 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
Effect of Variation of Chord and Span of Ailerons on Rolling and Yawing Moments at Several Angles of Pitch - Report N°343 / R. H. HEALD
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Effect of Variation of Chord and Span of Ailerons on Rolling and Yawing Moments at Several Angles of Pitch - Report N°343 [texte imprimé] / R. H. HEALD, Auteur ; D. H. STROTHER, Auteur ; B. H. MONISH, Auteur . - [s.d.] . - P.171-199 : ill. noir&blanc, photo, schémas. Langues : Anglais (eng) |
The Design of Plywood Webs for Airplane Wing Beams - Report N°344 / George W. TRAYER
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) The Design of Plywood Webs for Airplane Wing Beams - Report N°344 [texte imprimé] / George W. TRAYER, Auteur . - [s.d.] . - p.201-217 : ill. noir&blanc, tableaux. Langues : Anglais (eng) |
The Desing of Airplane Wing Ribs - Report N°345 / J. A. NEWLIN
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) The Desing of Airplane Wing Ribs - Report N°345 [texte imprimé] / J. A. NEWLIN, Auteur ; George W. TRAYER, Auteur . - [s.d.] . - p.219-272 : ill. noir&blanc, tableaux. Langues : Anglais (eng) |
Water Pressure Distribution on a Flying Boat Hull - Report N°346 / F. L. THOMPSON
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Water Pressure Distribution on a Flying Boat Hull - Report N°346 [texte imprimé] / F. L. THOMPSON, Auteur . - [s.d.] . - p.273-290 : ill. noir&blanc, tableaux. Langues : Anglais (eng) |
A Method of Calculating the Ultimate Strengh of Continuous Beams - Report N°347 / J. A. NEWLIN
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) A Method of Calculating the Ultimate Strengh of Continuous Beams - Report N°347 [texte imprimé] / J. A. NEWLIN, Auteur ; George W. TRAYER, Auteur . - [s.d.] . - p.291-318 : ill. noir&blanc, tableaux, photos. Langues : Anglais (eng) |
Strength of Welded Joints in Tubular Members for Aircraft - Report N°348 / H. L. WHITTEMORE
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) Strength of Welded Joints in Tubular Members for Aircraft - Report N°348 [texte imprimé] / H. L. WHITTEMORE, Auteur ; W. C. BRUEGGEMAN, Auteur . - [s.d.] . - p.319-359 : ill. noir&blanc, tableaux, photos. Langues : Anglais (eng) |
A Proof of the Theorem Regarding the Distribution of Lift Over the Span for Minimum Induced Drag - Report N°349 / William F. DURAND
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) A Proof of the Theorem Regarding the Distribution of Lift Over the Span for Minimum Induced Drag - Report N°349 [texte imprimé] / William F. DURAND, Auteur . - [s.d.] . - p.361-375. Langues : Anglais (eng) |
The Pressure Distribution over the Wings and Tail Surfaces of a PW-9 Pursuit Airplane in Flight - Report N°364 / Richard V. RHODE
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931)
contenu dans Sixteenth Reports of the National Advisory Committee for Aeronautics 1930 / National advisory committee for aeronautics (1931) The Pressure Distribution over the Wings and Tail Surfaces of a PW-9 Pursuit Airplane in Flight - Report N°364 [texte imprimé] / Richard V. RHODE, Auteur . - [s.d.] . - p.685-787 : ill. noir&blanc, photos, schémas. Langues : Anglais (eng) |
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