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  Partner: UNT Libraries Government Documents Department
 Serial/Series Title: NACA Aircraft Circulars
Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a figher-type airplane

Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a figher-type airplane

Date: April 1, 1945
Creator: Zalovcik, J. A. & Skoog, R. B.
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Investigation of the behavior of parallel two-dimensional air jets

Investigation of the behavior of parallel two-dimensional air jets

Date: November 1, 1944
Creator: Corrsin, Stanley
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Junkers Commercial Airplane G 31

Junkers Commercial Airplane G 31

Date: August 1, 1927
Creator: unknown
Description: The three engine Junkers commercial Airplane, type G 31 is a further development of the earlier G 24. It is an all metal low wing monoplane with a total engine output of 1100-1200 HP.
Contributing Partner: UNT Libraries Government Documents Department
Two 'Gloster' Airplanes : the 'Grouse II,' - Two-Seat Training Airplane. The 'Grebe II,' Single-Seat Fighter

Two 'Gloster' Airplanes : the 'Grouse II,' - Two-Seat Training Airplane. The 'Grebe II,' Single-Seat Fighter

Date: June 1, 1926
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
All-metal Junkers airplane, type F 13

All-metal Junkers airplane, type F 13

Date: May 1, 1926
Creator: unknown
Description: None
Contributing Partner: UNT Libraries Government Documents Department
Macchi M. 39 Seaplane: Single-Seat Racer with an 800 HP. Fiat "A-S2" Engine

Macchi M. 39 Seaplane: Single-Seat Racer with an 800 HP. Fiat "A-S2" Engine

Date: March 1, 1927
Creator: unknown
Description: The M. 39 was designed by Castoldi to compete in the Schneider Cup Race of 1926 (Norfolk, VA). It is a monoplane with engine mounted in the fuselage, resting on two wing and hull mounted floats.
Contributing Partner: UNT Libraries Government Documents Department
Dornier "Superwal" commercial seaplane with : two Rolls-Royce "Condor" 600 HP. engines

Dornier "Superwal" commercial seaplane with : two Rolls-Royce "Condor" 600 HP. engines

Date: February 1, 1927
Creator: unknown
Description: In November 1926, an exhibition flight of the Dornier giant flying boat was made for 3/4 of an hour. It was a larger version of the Dornier Wal, with a stepped hull, and wing stubs for lateral stability. It has a range of 1200 miles and is outfitted for baggage and 8 passengers.
Contributing Partner: UNT Libraries Government Documents Department
The Blackburn "Sprat": A Training Airplane Convertible into Landplane or Seaplane

The Blackburn "Sprat": A Training Airplane Convertible into Landplane or Seaplane

Date: July 1, 1926
Creator: unknown
Description: The Sprat is similar the Blackburn Swift and Dart models but is designed as a trainer. It is powered with a smaller 275 HP Rolls-Royce Falcon engine. It is a 2 seat biplane with equal sized upper and lower wings. It can quickly convert from a land to a seaplane.
Contributing Partner: UNT Libraries Government Documents Department
The Albatros L 72A : a German newspaper carrier with slotted wings

The Albatros L 72A : a German newspaper carrier with slotted wings

Date: June 1, 1926
Creator: unknown
Description: The Albatros 72A is a normal tractor biplane specifically designed to deliver newspapers by dropping them overboard in bundles for ground transport to pick up. It has a 42 ft. wingspan, and a 220 HP B.M.W. engine.
Contributing Partner: UNT Libraries Government Documents Department
The new De Havilland commercial airplane : the D.H. 66 with three Bristol "Jupiter" engines

The new De Havilland commercial airplane : the D.H. 66 with three Bristol "Jupiter" engines

Date: July 1, 1926
Creator: unknown
Description: The D.H. 66, constructed at Stag Lane Works of the De Haviland Aircraft Company built for Imperial Airways, Ltd. The fuselage has an all steel construction while the wings are made with box spars of wood and spruce ribs. It has a biplane tail and encloses the stabilizer trimming gear in a casing which serves to streamline the rear portion of the fuselage, but which is not part of the main structure. It weighs 9060 lbs. empty and 2500 lbs. after fueling with a total loaded weight of 14,700 lbs.
Contributing Partner: UNT Libraries Government Documents Department
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