Aerodynamic Characteristics Estimation of the High Speed Flight Demonstrator Phase II Using Flight Test Data

Purpose Aerodynamics of paragliders is very complicated aeroelastic phenomena. The purpose of this work is to quantify the amount of aerodynamic drag related to the flexible nature of a paraglider wing. Design/methodology/approach The laboratory testing on scaled models can be very difficult because of problems in the elastic similitude of such a structure. Testing of full-scale models in a large facility with a large full-scale test section is very expensive. The degradation of aerodynamic characteristics is evaluated from flight tests of the paraglider speed polar. All aspects of the identification such as pilot and suspension lines drag and aerodynamics of spanwise chambered wings are discussed. The drag of a pilot in a harness was estimated by means of wind tunnel testing, computational fluid dynamics (CFD) solver was used to estimating smooth wing lift and drag characteristics. Findings The drag related to the flexible nature of the modern paraglider wing is within the range of 4-30 per cent of the total aerodynamic drag depending on the flight speed. From the results, it is evident that considering only the cell opening effect is sufficient at a low-speed flight. The stagnation point moves forwards towards the nose during the high speed flight. This causes more pronounced deformation of the leading edge and thus increased drag. Practical implications This paper deals with a detailed analysis of specific paraglider wing. Although the results are limited to the specific geometry, the findings help in the better understanding of the paraglider aerodynamics generally. Originality/value The data obtained in this paper are not affected by any scaling problems. There are only few experimental results in the field of paragliders on scaled models. Those results were made on simplified models at very low Reynolds number. The aerodynamic drag characteristics of the pilot in the harness with variable angles of incidence and Reynolds numbers have not yet been published.

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Estimating Aerodynamic Characteristics of the ALFLEX Vehicle Using Flight Test Data.

The Journal of the Japan Society of Aeronautical Engineering ◽

10.2322/jjsass1969.46.29 ◽

1998 ◽

Vol 46 (528) ◽

pp. 29-36

Author(s):

Masaaki YANAGIHARA ◽

Masashi SHIGEMI ◽

Noriaki OKADA ◽

Takanobu SUITO

Keyword(s):

Test Data ◽

Flight Test ◽

Aerodynamic Characteristics

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Estimation of Aerodynamic Characteristics from Flight-Test Data. (3rd Report). Explanatory Variables Error Method Corresponding to Output Error Method.

The Journal of the Japan Society of Aeronautical Engineering ◽

10.2322/jjsass1969.41.104 ◽

1993 ◽

Vol 41 (469) ◽

pp. 104-113

Author(s):

Osamu KOBAYASHI

Keyword(s):

Test Data ◽

Flight Test ◽

Aerodynamic Characteristics ◽

Explanatory Variables ◽

Output Error ◽

Error Method

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