Cover Image

Hydrodynamic and aerodynamic tests of four models of outboard floats N.A.C.A. models 51-A, 51-B, 51-C, and 51-D.

Bibliographic Details
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document eBook
Language:	English
Published:	[Washington] : [s.n.], 1938.
Subjects:	Aeronautics > Research. Airplanes. Statistics. Aeronautics.
Online Access:	Electronic resource (PDF)

Similar Items

Aerodynamic drag of five models of side floats, N.A.C.A. models 51-E, 51-F, 51-G, 51-H, and 51-J.
Published: (1938)

Hydrodynamic and aerodynamic tests of models of flyingboat hulls designed for low aerodynamic drag.
Published: (1938)

N.A.C.A. Stall-warning indicator.
Published: (1938)

Executive Agreement Series, No. 51 : Pilot Licenses to Operate Civil Aircraft, Arrangement Between the United States of America and Norway.
Published: (1933)

Damping formulas and experimental values of damping in flutter models.
Published: (1940)

A new method of studying the flow of the water along the bottom of a model of a flying-boat hull.
Published: (1940)

Hydrodynamic and aerodynamic tests of a family of models of seaplane floats with varying angles of dead rise, N. A. C. A. models 57-A, 57-B, and 57-C.
Published: (1939)

Civil Air Regulations, Part 51. - Ground Instructor Rating.
Published: (1940)

A study of unsymmetrical-loading conditions.
Published: (1940)

Contribution to the problem of airfoils spanning a free jet.
Published: (1936)

Work Materials No. 51 : The Code Making Program the NRA in the Territories.
Published: (1936)

Full-scale wind-tunnel and flight tests of a Fairchild 22 airplane equipped with external-airfoil flaps.
Published: (1937)

Design of N.A.C.A. cowlings for radial air℗--cooled engines.
Published: (1938)

Flight tests of an airplane showing dependence of the maximum lift coefficient on the test conditions.
Published: (1937)

Fatigue testing of wing beams by resonance method.
Published: (1938)

Performance characteristics of Venturi tubes used in aircraft for operating air-driven gyroscopic instruments.
Published: (1937)

Flight measurements of dynamic longitudinal stability of several airplanes and correlation of measurements with pilots' observations of handling characteristics.
Published: (1936)

Maximum forces applied by pilots to wheel-type controls.
Published: (1937)

Chief characteristics and advantages of tailless airplanes.
Published: (1936)

Flow observations with tufts and lampblack of stalling of 4 typical airfoil sections in N.A.C.A. variable℗--density tunnel.
Published: (1938)

Wind℗-tunnel investigation of rectangular and tapered N. A. C. A. 23012 wings with plain ailerons and full℗-span split flaps.
Published: (1938)

Experiment station record, Volume 51.
Published: (1924)

A generalized vortex theory of the screw propeller and its application.
Published: (1040)

Hydrodynamic and aerodynamic tests of models of floats for single℗--float seaplanes. N. A. C. A. models 41-D. 41-E. 61-A. 73 and 73-A.
Published: (1938)

Hydrodynamic tests in N. A. C. A. tank of model of hull of Short Calcutta flying boat.
Published: (1937)

Proceedings of U.S. National Museum, Vol. 51.
Published: (1916)

An investigation of sheet-stiffener panels subjected to compression loads with particular reference to torsionally weak stiffeners.
Published: (1940)

Flight investigation of reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design.
Published: (1938)

The measurement of field of view from airplane cockpits.
Published: (1934)

This Week in Defense, 1941, No. 51.
Published: (1941)

Tests of N.A.C.A. 0009, 0012, and 0018 airfoils in full-scale tunnel.
Published: (1938)

Special Orders No. 51, Mar. 2, 1934.
Published: (1934)

Special Orders No. 51, Mar. 3, 1933.
Published: (1933)

Special Orders No. 51, Mar. 4, 1937.
Published: (1937)

Special Orders No. 51, Mar. 3, 1938.
Published: (1938)

Special Orders No. 51, Mar. 3, 1933.
Published: (1933)

In matter of suspension of Western Classification No. 51, I.C.C. No. 9.
Published: (1912)

The drag of inflatable rubber de-icers.
Published: (1938)

Loads imposed on intermediate frames of stiffened shells.
Published: (1939)

Status of wing flutter.
Published: (1936)