FIELD: determination of parameters of flight of flying vehicles or parameters of flow in wind tunnels. SUBSTANCE: pitot-static tube is made in form of two prismatic bodies located coaxially; their section has form of equilateral triangle with vertices shifted through angle of 60 deg; lateral faces of prisms are provided with inlet holes connected with pipe unions by means of pneumatic lines. Specific feature of this pitot-static tube consists in convex lateral faces of prisms at curvature radius R found from relationship R/r>1, where r is radius of circle drawn through vertices of triangle angles located in sections of prisms. Such construction of pitot-static tube makes it possible on one side to minimize effect of Reynolds number on pressure measurements and on other side to enhanced sensitivity of instrument due to rise of derivative of pressure being measured by downwash angle, thus considerably reducing instrument errors. EFFECT: reduction of instrument errors. 3 dwg , 1 tbl
Title | Year | Author | Number |
---|---|---|---|
PITOT-STATIC TUBE | 1997 |
|
RU2121667C1 |
AIR PRESSURE TRANSDUCER | 1998 |
|
RU2135971C1 |
AIR PRESSURE PICKUP | 0 |
|
SU1809341A1 |
HIGH-PRESSURE TUBE ( VARIANTS ) | 1998 |
|
RU2152042C1 |
AIR PRESSURE INTAKE | 2013 |
|
RU2542791C1 |
FUSELAGE PITOT-STATIC TUBE WITH A STRUT | 1997 |
|
RU2157980C2 |
PROPELLER BLADE | 1996 |
|
RU2123453C1 |
AERODYNAMIC PROFILE OF LOAD-BEARING MEMBER OF FLYING VEHICLE | 1996 |
|
RU2098321C1 |
PITOT-STATIC PROBE | 0 |
|
SU1809340A1 |
PITOT-STATIC PROBE | 0 |
|
SU1809339A1 |
Authors
Dates
1998-07-10—Published
1996-08-12—Filed