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Seventeenth Report of the National Advisory Committee for Aeronautics 1931 / National advisory committee for aeronautics (1932)
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Aerodynamic Characteristics of Circular-Arc Airfoils at High Speeds - Report N°365 / L. J. BRIGGS
The Comparative Performance of Superchargers - Report N°384 / Oscar W. SCHEY
Wind Tunnel Tests on Airfoil Boundary Layer Control Using a Backward-Opening Slot - Report N°385 / Oscar W. SCHEY
Maneuverability Investigation of an F6C-4 Fighting Airplane - Report N°386 / C. H. DEARBORN
The Vertical Wind Tunnel of the National Advisory Committee for Aeronautics - Report N°387 / Carl J. WENZINGER
Investigation of the Diaphragm-Type Pressure Cell - Report N°388 / Theodore THEODORSEN
The Effect of Small Angles of Yaw and Pitch on the Characteristics of Airplane Propellers - Report N°389 / Hugh B. FREEMAN
The Effect of Valve Timing upon the Performance of a Supercharged Engine at Altitude and an Unsupercharged Engine at Sea Level - Report N°390 / Oscar W. SCHEY
The Aerodynamic Characteristics of Eight Very Thick Airfoils from Tests in the Variable Density Wind Tunnel - Report N°391 / Eastman N. JACOBS
Reduction of Turbulence in Wind Tunnels - Report N°392 / H. L. DRYDEN
Span-Load Distribution as a Factor in Stability in Roll - Report N°393 / Montgomery KNIGHT
Airship Model in the Variable Density Wind Tunnel - Report N°394 / Ira H. ABBOTT
A New Principle of Sound Frequency Analysis - Report N°395 / Theodore THEODORSEN
Hydraulics of Fuel Injection Pumps for Compression-Ignition Engines - Report N°396 / A. M. ROTHROCK
The Drag Characteristics of Several Airships Determined by Deceleration Tests - Report N°397 / F. L. THOMPSON
Investigation of Damping Liquids for Aircraft Instruments-II - Report N°398 / M. R. HOUSEMAN
Flame Movement and Pressure Development in an Engine Cylinder - Report N°399 / Charles F. MARVIN
On the Theory of Wing Sections with Particular Reference to the Lift Distribution - Report N°383 / Theodore THEODORSEN
Elastic Instability of Members Having Sections Common in Aircraft Construction - Report N°382 / George W. TRAYER
Dynamic and Flight Test on Rubber-Cord and Oleo-Rubber-Disk Landing Gears for an F6C-4 Airplane - Report N°366 / William C. PECK
Pressure Distribution Over a Thick, Tapered and Twisted Monoplane Wing Model-NACA 81-J - Report N°367 / Carl J. WENZINGER
A New Chart for Estimating the Absolute Ceiling of an Airplane - Report N°368 / Walter S. DIEHL
Maneuverability Investigation of the F6C-3 Airplane with Special Flight Instruments - Report N°369 / C. H. DEARBORN
Effect of Variation of Chord and Span of Ailerons on Hinge Moments at Several Angles of Pitch - Report N°370 / B. H. MONISH
Present Statuts of Aircraft Instruments - Report N°371 / Subcommittee on Instruments
The Gaseous Explosive Reaction - The effect of Pressure on the Propagation of the Reaction Zone and upon the Rate of Molecular Transformation - Report N°372 / F. W. STEVENS
Coefficients of Discharge of Fuel Injection Nozzles for Compression-Ignition Engines - Report N°373 / A. G. GELALLES
The Automotive Ignition Coil - Report N°374 / T. H. DARNELL
Full-Scale Tests of Metal Propellers at High Tip Speeds - Report N°375 / Donald H. WOOD
Some Approximate Equations for the Standard Atmosphere - Report N°376 / Walter S. DIEHL
A Method of Flight Measurement of Spins - Report N°377 / Hartley A. SOULE
Comparison of Full-Scale Propellers Having RAF-6 and Clark Y Airfoil Sections - Report N°378 / Hugh B. FREEMAN
Rolling Moments Due to Rolling and Yaw for Four Wing Models in Rotation - Report N°379 / Montgomery KNIGHT
Pressure Distribution Over the Fuselage of a Pw-9 Pursuit Airplane in Flight - Report N°380 / Richard V. RHODE
Static, Drop, and Flight Tests on Musselman Type Airwheels - Report N°381 / William C. PECK
The Aerodynamic Characteristics of a Slotted Clark Y Wing as Affected by the Auxiliary Airfoil Position - Report N°400 / Carl J. WENZINGER
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| Code-barres | Cote | Support | Localisation | Section | Disponibilité |
|---|---|---|---|---|---|
| 89 | 629.11 NAT | Rapports | Centre de documentation | Bibliothèque AAE | Disponible |
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