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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Aircraft Circulars
 Collection: Technical Report Archive and Image Library
The Shackleton-Murray SM-1 light airplane  : a two-place high-wing monoplane

The Shackleton-Murray SM-1 light airplane : a two-place high-wing monoplane

Date: June 1, 1933
Creator: NACA
Description: None
Contributing Partner: UNT Libraries Government Documents Department
A Concise Theoretical Method for Profile-Drag Calculation; Advance Report

A Concise Theoretical Method for Profile-Drag Calculation; Advance Report

Date: February 1, 1944
Creator: Nitzberg, Gerald E.
Description: In this report a method is presented for the calculation of the profile drag of airfoil sections. The method requlres only a knowledge of the theoretical velocity distribution and can be applied readily once this dlstribution is ascertained. Comparison of calculated and experimental drag characteristics for several airfoils shows a satisfactory agreement. Sample calculatlons are included.
Contributing Partner: UNT Libraries Government Documents Department
The propeller and cooling-air-flow characteristics of a twin-engine airplane model equipped with NACA D(sub S)-type cowlings and with propellers of NACA 16-series airfoil sections

The propeller and cooling-air-flow characteristics of a twin-engine airplane model equipped with NACA D(sub S)-type cowlings and with propellers of NACA 16-series airfoil sections

Date: September 1, 1944
Creator: Pepper, Edward
Description: None
Contributing Partner: UNT Libraries Government Documents Department
The Hanriot-Biche 110 C1 airplane (French) : an all-metal low-wing pursuit monoplane

The Hanriot-Biche 110 C1 airplane (French) : an all-metal low-wing pursuit monoplane

Date: July 1, 1933
Creator: Rabion, Rene
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Experiments on drag of revolving disks, cylinders and streamline rods at high speeds

Experiments on drag of revolving disks, cylinders and streamline rods at high speeds

Date: June 1, 1944
Creator: Regier, Arthur
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Albatros commercial Airplane L 73

Albatros commercial Airplane L 73

Date: September 1, 1926
Creator: Ruhl, Karl & Wiederhold, Hasso
Description: The Albatros was a two engine commercial biplane carrying 2 pilots, eight passengers, and 160 KG of baggage. The framework is metal, the wings having plywood and fabric over the steel tubing. The L 73 was the first 2 engine biplane to be made in Germany.
Contributing Partner: UNT Libraries Government Documents Department
Bleriot-Spad 91 Airplane (French) : pursuit single-seater, type "Jockey"

Bleriot-Spad 91 Airplane (French) : pursuit single-seater, type "Jockey"

Date: May 1, 1928
Creator: SOCIETE BLERIOT-AERONAUTIQUE
Description: This aircraft has announced a speed of 270 km per hour at 4000 m. It is of all metal construction.
Contributing Partner: UNT Libraries Government Documents Department
The "K 47" of the A.B. Flygindustri : An Armored Pursuit Monoplane

The "K 47" of the A.B. Flygindustri : An Armored Pursuit Monoplane

Date: August 1, 1929
Creator: Schulz, R
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Albessard "Triavion" Airplane (French) : A Two-Seat Tandem Monoplane

Albessard "Triavion" Airplane (French) : A Two-Seat Tandem Monoplane

Date: January 1, 1929
Creator: Serryer, J
Description: Autostability is the watchword of this tandem monoplane. The tandem design causes a natural flat flight pattern. It can also land and take off from very short runways.
Contributing Partner: UNT Libraries Government Documents Department
Avia pursuit airplane B.H. 21

Avia pursuit airplane B.H. 21

Date: November 1, 1926
Creator: Serryer, J
Description: Built by the 'Czecho-Slovakian' aircraft factory, AVIA, the B.H. 21, has a top speed of 250 MPH, and carries 120 kg of gasoline and 20 kg of oil, giving it a radius of action of 600-650 km. It is equipped with a Hispano-Suiza engine capable of 300 HP.
Contributing Partner: UNT Libraries Government Documents Department