FIELD: aeronautical engineering. SUBSTANCE: parameters of flow near flying vehicle are measured and aerodynamic parameter which changes under action of screen is formed. Parameters of flow, motion and configuration of flying vehicle are determined. Flight altitude is determined from calibration relationship from indicated parameters formed in flight experiment. EFFECT: enhanced efficiency. 3 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
AMPHIBIAN | 1997 |
|
RU2135394C1 |
FIREPROOF HYDROPLANE | 1991 |
|
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SEAPLANE | 1993 |
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SEAPLANE FUEL TANK VENTING SYSTEM | 1992 |
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ENGINE CONTROL UNIT | 1993 |
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0 |
|
SU1782220A3 | |
AMPHIBIA | 1997 |
|
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SEAPLANE | 2001 |
|
RU2223200C2 |
SEAPLANE ULTRA-LOW ALTITUDE CAPACITANCE-TYPE SENSOR | 2001 |
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RU2196077C2 |
METHOD OF MEASUREMENT OF EXTRA LOW FLIGHT ALTITUDE OF AIRCRAFT, MAINLY SEAPLANE ABOVE WATER SURFACE AND PARAMETERS OF SEA SWELL | 1999 |
|
RU2183010C2 |
Authors
Dates
1995-07-25—Published
1992-03-24—Filed