Wind℗--tunnel and flight tests of slot-lip ailerons.
| Corporate Author: | United States. National Advisory Committee for Aeronautics |
|---|---|
| Format: | Government Document eBook |
| Language: | English |
| Published: |
[Washington] :
[s.n.],
1937.
|
| Subjects: | |
| Online Access: | Electronic resource (PDF) |
Similar Items
Comparison of profile-drag and boundary℗--layer measurements obtained in flight and in the full℗--scale wind tunnel.
Published: (1939)
Published: (1939)
Preliminary tests in the N. A. C. A. free℗-spinning wind tunnel.
Published: (1935)
Published: (1935)
Full-scale wind℗--tunnel and flight tests of Fairchild 22 airplane equipped with zap flap and zap ailerons.
Published: (1937)
Published: (1937)
Wind℗--tunnel investigation of tapered wings with ordinary ailerons and partial℗--span split flaps.
Published: (1937)
Published: (1937)
Wind℗--tunnel investigation of wings with ordinary ailerons and full-span external-airfoil flaps.
Published: (1937)
Published: (1937)
Experiments on a slotted wing.
Published: (1939)
Published: (1939)
Wind-tunnel tests of 2-engine airplane model as preliminary study of flight conditions arising on failure of one engine.
Published: (1938)
Published: (1938)
Breda wind tunnel.
Published: (1939)
Published: (1939)
Air flow around finned cylinders.
Published: (1936)
Published: (1936)
Wind-tunnel tests of Clark Y wing with Maxwell leading-edge slots.
Published: (1937)
Published: (1937)
Flight and wind-tunnel tests of XBM-1 dive bomber.
Published: (1938)
Published: (1938)
The 5- by 7-meter wind tunnel of the DVL.
Published: (1936)
Published: (1936)
Investigations and experiments in Guidonia supersonic wind tunnel.
Published: (1939)
Published: (1939)
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)
Systematic airfoil tests in large wind tunnel of DVL.
Published: (1938)
Published: (1938)
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)
Wind℗--tunnel tests of 10-foot-diameter gyroplane rotor.
Published: (1935)
Published: (1935)
Wind-tunnel investigation of an N. A. C. A. 23030 airfoil with various arrangements of slotted flaps.
Published: (1940)
Published: (1940)
Comparative flight and full-scale wind℗--tunnel measurements of the maximum lift of airplane.
Published: (1937)
Published: (1937)
Flight investigation of lateral control characteristics of short wide ailerons and various spoilers with different amounts of wing dihedral.
Published: (1934)
Published: (1934)
Aerodynamic characteristics of large number of airfoils tested in variable-density wind tunnel.
Published: (1937)
Published: (1937)
Wind-tunnel investigation of N. A. C. A. 23012 airfoil with slotted flap and 3 types of auxiliary flap.
Published: (1938)
Published: (1938)
Flight investigation of reduction of aileron operating force by means of fixed tabs and differential linkage, with notes on linkage design.
Published: (1938)
Published: (1938)
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)
Tests in the gust tunnel of a model of the XBM-1 airplane.
Published: (1939)
Published: (1939)
Pioneer wind tunnels.
Published: (1935)
Published: (1935)
Wind℗--tunnel research comparing lateral control devices, particularly at high angles of attack : XIII - Auxiliary airfoils used as external ailerons.
Published: (1934)
Published: (1934)
Full℗--scale wind℗--tunnel and flight tests of Fairchild 22 airplane equipped with Fowler flap.
Published: (1936)
Published: (1936)
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)
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)
Measurement of the forces acting on gliders in towed flight.
Published: (1940)
Published: (1940)
Wind-tunnel tests of carburetor-intake rams.
Published: (1938)
Published: (1938)
Full-scale tests of a new type N. A. C. A. nose-slot cowling.
Published: (1936)
Published: (1936)
Wind℗--tunnel tests of Clark Y wing having split flaps with gaps.
Published: (1938)
Published: (1938)
Experimental investigation of wind-tunnel interference on the downwash behind an airfoil.
Published: (1937)
Published: (1937)
Aileron effectiveness : Wind tunnel tests of U.S.A. 35 (half-span) airfoil with skewed ailerons (Airplane Section report).
Published: (1924)
Published: (1924)
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)
Fuselage-drag tests in the variable-density wind tunnel : Streamline bodies of revolution, fineness ratio of 5.
Published: (1937)
Published: (1937)
Flight comparison of conventional ailerons on rectangular wing and of conventional and floating wing℗--tip ailerons on tapered wing.
Published: (1937)
Published: (1937)