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Works matching IS 25452835 AND DT 2021 AND VI 2021 AND IP 3

Results: 6

1

A TWO-POINT APPROXIMATION APPROACH TO DETERMINING AIRCRAFT AERODYNAMIC FORCE COEFFICIENTS FOR A MAXIMAL<DURATION HORIZONTAL FLIGHT.

Published in:

Transactions on Aerospace Research, 2021, v. 2021, n. 3, p. 71, doi. 10.2478/tar-2021-0018

By:

Goncharenko, Andriy Viktorovich

Publication type:

Article

2

A MATHEMATICAL MODEL FOR CONTROLLING A QUADROTOR UAV.

Published in:

Transactions on Aerospace Research, 2021, v. 2021, n. 3, p. 58, doi. 10.2478/tar-2021-0017

By:

Kowalik, Rafał;
Łusiak, Tomasz;
Novak, Andrej

Publication type:

Article

3

IMPACT OF LOAD RETENTION ON AIRCRAFT ENGINE PARTS UNDER REAL FLIGHT CYCLE CONDITIONS IN SERVICE LIFE MONITORING.

Published in:

Transactions on Aerospace Research, 2021, v. 2021, n. 3, p. 47, doi. 10.2478/tar-2021-0016

By:

Yepifanov, sergiy;
Brunak, Andrii

Publication type:

Article

4

NUMERICAL SIMULATION OF THE EXIT TEMPERATURE PATTERN OF AN AIRCRAFT ENGINE USING A TEMPERATURE- DEPENDENT TURBULENT SCHMIDT NUMBER.

Published in:

Transactions on Aerospace Research, 2021, v. 2021, n. 3, p. 34, doi. 10.2478/tar-2021-0015

By:

Kravchenko, Igor F.;
Kozel, Dmytro V.;
Yevsieiev, Serhii A.

Publication type:

Article

5

NUMERICAL INVESTIGATION OF DETONATION PROPAGATION THROUGH SMALL ORIFICE HOLES.

Published in:

Transactions on Aerospace Research, 2021, v. 2021, n. 3, p. 17, doi. 10.2478/tar-2021-0014

By:

Vashishtha, Ashish;
Callaghan, Dean;
Nolan, Cathal;
Deiterding, Ralf

Publication type:

Article

6

ENHANCED FEATURE EXTRACTION ALGORITHMS USING OSCILLATORY-MODE PULSED EDDY CURRENT TECHNIQUES FOR AIRCRAFT STRUCTURE INSPECTION.

Published in:

Transactions on Aerospace Research, 2021, v. 2021, n. 3, p. 1, doi. 10.2478/tar-2021-0013

By:

Lysenko, Iuliia;
Kuts, Yurii;
Protasov, Anatoliy;
Redka, Mykhailo;
Uchanin, Valentin

Publication type:

Article