You limited your search to:

  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Technical Memorandums
 Collection: National Advisory Committee for Aeronautics Collection
Pressure Distribution on Joukowski Wings

Pressure Distribution on Joukowski Wings

Date: December 1, 1979
Creator: Blumenthal, O.
Description: The hydrodynamics and mathematical models as applied to the potential flow about a Joukowski wing are presented.
Contributing Partner: UNT Libraries Government Documents Department
Graphic Construction of Joukowski Wings

Graphic Construction of Joukowski Wings

Date: December 1, 1979
Creator: Trefftz, E.
Description: A plot of the cross sectional outline of a Joukowski wing is presented.
Contributing Partner: UNT Libraries Government Documents Department
Flight experiences and tests on two airplanes with suction slots

Flight experiences and tests on two airplanes with suction slots

Date: January 1, 1950
Creator: Stueper, BY
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Theoretical investigation of drag reduction in maintaining the laminar boundary layer by suction

Theoretical investigation of drag reduction in maintaining the laminar boundary layer by suction

Date: June 1, 1947
Creator: Ulrich, A.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Sixth meeting of the members of the German Scientific Association for Aeronautics

Sixth meeting of the members of the German Scientific Association for Aeronautics

Date: April 1, 1921
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Resume of the theory of naval and aerial propulsive propellers and of airplanes in the rectilinear flight

Resume of the theory of naval and aerial propulsive propellers and of airplanes in the rectilinear flight

Date: April 1, 1921
Creator: Rateau, A
Description: Though dissimilar, these two subjects have been united because they have some points in common. The computation of the movement of an airplane can only be correctly established if we are in a position to know exactly the thrust and resisting torque of the propeller for the various values of slip, which may vary greatly according to circumstance. The first part of the work concerns propellers and introduces as a fundamental variable, the true slip (delta) with respect to the effective pitch, which is the advance per revolution of the propeller corresponding to no thrust. The second part deals with characteristic curves of an airplane.
Contributing Partner: UNT Libraries Government Documents Department
The 1000 HP traffic airplane of the Zeppelin Works in Staaken

The 1000 HP traffic airplane of the Zeppelin Works in Staaken

Date: September 1, 1921
Creator: Rohrbach, A K
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Recent developments in light alloys

Recent developments in light alloys

Date: November 1, 1920
Creator: Woodward, R W
Description: This report is intended to cover the progress that has been made in both the manufacture and utility of light alloys in the United States since the first part of 1919. Duralumin is extensively discussed both as to manufacture and durability.
Contributing Partner: UNT Libraries Government Documents Department
The Rumpler passenger airplane

The Rumpler passenger airplane

Date: March 1, 1921
Creator: Langsdorff, Werner V
Description: This report details the Rumpler Limousine which was a further development of the well known type 5 A 2. The fuselage, engine, cabin, wings, controls, and landing gear are all discussed.
Contributing Partner: UNT Libraries Government Documents Department
Development of aeronautical engines by the Army and Navy

Development of aeronautical engines by the Army and Navy

Date: March 3, 1921
Creator: unknown
Description: Different aircraft engines are categorized as being of interest to only the Army or Navy or to both armed services. A listing of the different engines is presented along with some statistics, namely, horsepower.
Contributing Partner: UNT Libraries Government Documents Department
FIRST PREV 1 2 3 4 5 NEXT LAST