Investigations and experiments in Guidonia supersonic wind tunnel.
| Corporate Author: | United States. National Advisory Committee for Aeronautics |
|---|---|
| Format: | Government Document eBook |
| Language: | English |
| Published: |
[Washington] :
[s.n.],
1939.
|
| Subjects: | |
| Online Access: | Electronic resource (PDF) |
Similar Items
Breda wind tunnel.
Published: (1939)
Published: (1939)
The 5- by 7-meter wind tunnel of the DVL.
Published: (1936)
Published: (1936)
Systematic airfoil tests in large wind tunnel of DVL.
Published: (1938)
Published: (1938)
Wind℗--tunnel tests of 10-foot-diameter gyroplane rotor.
Published: (1935)
Published: (1935)
Aerodynamic characteristics of large number of airfoils tested in variable-density wind tunnel.
Published: (1937)
Published: (1937)
Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails : 2. Mass distributed along fuselage.
Published: (1937)
Published: (1937)
Determination of boundary-layer transition on 3 symmetrical airfoils in N. A. C. A. full℗--scale wind tunnel [National Advisory Committee for Aeronautics].
Published: (1938)
Published: (1938)
Tests in the gust tunnel of a model of the XBM-1 airplane.
Published: (1939)
Published: (1939)
Wind-tunnel tests of carburetor-intake rams.
Published: (1938)
Published: (1938)
Wind-tunnel investigation of ordinary and split flaps on airfoils of different profile.
Published: (1935)
Published: (1935)
Wind℗--tunnel and flight tests of slot-lip ailerons.
Published: (1937)
Published: (1937)
Pioneer wind tunnels.
Published: (1935)
Published: (1935)
Interference of wing and fuselage from tests of 17 combinations in N. A. C. A. variable-density tunnel combinations with special juncture.
Published: (1938)
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)
Published: (1938)
Tests of N-85, N-86, and N-87 airfoil sections in 11-inch high-speed wind tunnel.
Published: (1938)
Published: (1938)
Experimental Results with Airfoils Tested in the High-Speed Tunnel at Guidonia.
Published: (1940)
Published: (1940)
Tests of Related Forward-Camber Airfoils in the Variable-Density Wind Tunnel.
Published: (1937)
Published: (1937)
Experiments on a slotted wing.
Published: (1939)
Published: (1939)
Comparison of profile-drag and boundary℗--layer measurements obtained in flight and in the full℗--scale wind tunnel.
Published: (1939)
Published: (1939)
The Dornier wind tunnel.
Published: (1938)
Published: (1938)
Wind-tunnel tests of Clark Y wing with Maxwell leading-edge slots.
Published: (1937)
Published: (1937)
Wind-tunnel investigation of N. A. C. A. 23012 airfoil with various arrangements of slotted flaps.
Published: (1939)
Published: (1939)
Wind-tunnel investigation of N. A. C. A. 23021 airfoil with various arrangements of slotted flaps.
Published: (1939)
Published: (1939)
Tests in variable℗--density wind tunnel of related airfoils having the maximum camber unusually far forward.
Published: (1935)
Published: (1935)
Wind℗--tunnel tests of wing flaps suitable for direct control of glide-path angle.
Published: (1936)
Published: (1936)
An experimental investigation of the normal acceleration of an airplane model in a gust.
Published: (1939)
Published: (1939)
Free-spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails, III. Mass distributed along the wings.
Published: (1938)
Published: (1938)
Experimental Results with Airfoils Tested in the High-Speed Tunnel at Guidonia.
Published: (1940)
Published: (1940)
Wind℗--tunnel investigation of N. A. C. A. 23012, 23021, and 23030 airfoils with various sizes of split flap.
Published: (1939)
Published: (1939)
Wind-tunnel investigation of N. A. C. A. 23012 airfoil with slotted flap and 3 types of auxiliary flap.
Published: (1938)
Published: (1938)
Investigation of full℗--scale split trailing-edge wing flaps with various chords and hinge locations.
Published: (1935)
Published: (1935)
Full℗--scale wind℗--tunnel and flight tests of Fairchild 22 airplane equipped with Fowler flap.
Published: (1936)
Published: (1936)
Tests of N. A. C. A. airfoils in variable-density wind tunnel, series 230.
Published: (1936)
Published: (1936)
Wind℗--tunnel research comparing lateral control devices, particularly at high angles of attack : XIII - Auxiliary airfoils used as external ailerons.
Published: (1934)
Published: (1934)
Wind-Tunnel Research Comparing Lateral Control Devices, Particularly at High Angles of Attack : XII - Upper-Surface Ailerons on Wings with Split Flaps.
Published: (1934)
Published: (1934)
Free℗--spinning wind-tunnel tests of low-wing monoplane with systematic changes in wings and tails : 4, Effect of center-of℗--gravity location.
Published: (1939)
Published: (1939)
Full-scale wind℗--tunnel and flight tests of Fairchild 22 airplane equipped with zap flap and zap ailerons.
Published: (1937)
Published: (1937)
Tests in variable℗-density wind tunnel of N. A. C. A. 23012 airfoil with plain and split flaps.
Published: (1938)
Published: (1938)
Wind-tunnel investigation of ground effect on wings with flaps.
Published: (1939)
Published: (1939)
Full-scale wind℗--tunnel tests to determine satisfactory location for service pitot-static tube on low-wing monoplane.
Published: (1936)
Published: (1936)