NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Twenty-First Annual Report of the National Advisory Committee for Aeronautics: 1935 - Including Technical Reports Nos. 508 to 541Report includes the National Advisory Committee for Aeronautics letter of submittal to the President, Congressional report, summaries of the committee's activities and research accomplished, bibliographies, and financial report.
Document ID
19930091580
Acquisition Source
Headquarters
Document Type
Other - NACA Annual Report
Authors
Joseph S Ames (National Advisory Committee for Aeronautics Washington, United States)
Date Acquired
September 6, 2013
Publication Date
January 7, 1936
Publication Information
Publisher: National Advisory Committee for Aeronautics
Subject Category
Aeronautics (General)
Report/Patent Number
NACA-AR-21
Accession Number
93R20870
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19930091582See AlsoGeneral Equations for the Stress Analysis of Rings19930091603See AlsoCharacteristics of the N. A. C. A. 23012 Airfoil From Tests in the Full-Scale and Variable-Density Tunnels19930091581See AlsoAnalysis of 2-Spar Cantilever Wings With Special Reference to Torsion and Load Transference19930091585See AlsoSome Factors Affecting Combustion in an Internal-Combustion Engine19930091588See AlsoThe Measurement of the Field of View from Airplane Cockpits19930091589See AlsoPotential Flow About Elongated Bodies of Revolution19930091613See AlsoInterference of Wing and Fuselage From Tests of 209 Combinations in the N. A. C. A. Variable-Density Tunnel19930091614See AlsoAerodynamic Characteristics of Wings With Cambered External-Airfoil Flaps, Including Lateral Control, With a Full-Span Flap19930091583See AlsoWind-Tunnel Research Comparing Lateral Control Devices Particularly at High Angles of Attack: XIII-Auxiliary Airfoils Used as External Ailerons19930091591See AlsoThe Drag of Airplane Wheels, Wheel Fairings, and Landing Gears II: Nonretractable and Partly Retractable Landing Gears19930091584See AlsoThe Effect of Baffles on the Temperature Distribution and Heat-Transfer Coefficients of Finned Cylinders19930091592See AlsoSpinning Characteristics of Wings I: Rectangular Clark Y Monoplane Wing19930091596See AlsoThe Influence of Wing Setting on the Wing Load and Rotor Speed of a PCA-2 Autogiro as Determined in Flight19930091593See AlsoA Comparison of Fuel Sprays from Several Types of Injection Nozzles19930091597See AlsoA Turbulence Indicator Utilizing the Diffusion of Heat19930091594See AlsoAn Analysis of Longitudinal Stability in Power-Off Flight With Charts for Use in Design19930091598See AlsoSome Effects of Injection Advance Angle, Engine-Jacket Temperature, and Speed on Combustion in a Compression-Ignition Engine19930091612See AlsoInvestigation of Full-Scale Split Trailing-Edge Wing Flaps With Various Chords and Hinge Locations19930091599See AlsoNoise from Two-Blade Propellers19930091600See AlsoAir Flow in a Separating Laminar Boundary Layer19930091601See AlsoReduction of Hinge Moments of Airplane Control Surfaces By Tabs19930091602See AlsoA Flight Investigation of the Spinning of the F4B-2 Biplane with Various Loads and Tail Surfaces19930091604See AlsoThe Effect of Water Vapor on Flame Velocity in Equivalent CO-O<sub>2</sub> Mixtures19930091605See AlsoThe Soap-Bubble Method of Studying the Combustion of Mixtures of CO and O<sub>2</sub>19930091606See AlsoDistribution and Regularity of Injection From a Multicylinder Fuel-Injection Pump19930091607See AlsoAerodynamic Characteristics of a Wing With Fowler Flaps Including Flap Loads, Downwash, and Calculated Effect on Take-Off19930091609See AlsoHydrogen as an Auxiliary Fuel in Compression-Ignition Engines19930091608See AlsoWind-Tunnel Tests of a 10-Foot-Diameter Gyroplane Rotor19930091610See AlsoTests in the Variable-Density Wind Tunnel of Related Airfoils Having the Maximum Camber Unusually Far Forward19930091586See AlsoExperimental Investigation of the Robinson-Type Cup Anemometer19930091587See AlsoFull-Scale Wind-Tunnel Tests of a PCA-2 Autogiro Rotor19930091590See AlsoFlight Investigation of Lateral Control Devices for Use With Full-Span Flaps19930091595See AlsoThe Drag of Airplane Wheels, Wheel Fairings, and Landing Gears: III19930091611See AlsoAltitude-Pressure Tables Based on the United States Standard Atmosphere
No Preview Available