Results 251 to 260 of about 16,981 (316)
Performance of a Swept Leading Edge Rotor of the Supersonic Type with Mixed Flow
, 1953 Arthur W Goldstein, R. L. Schacht
openalex +1 more source
Control of flow deflection angle around the corner using microjet array. [PDF]
Sci RepNakadori Y +4 more
europepmc +1 more source
Low-overload internal ballistics in UAV ejection using multiple time-sequenced compressed-air chambers. [PDF]
Sci RepLi T +5 more
europepmc +1 more source
Characteristics of Aerodynamic Five-Hole-Probes in Transonic and Supersonic Flow Regimes
, 1981 Torsten Fransson, O. Sari
openalex +1 more source
Experimental and Calculated Flow Fields Produced by Airplanes Flying at Supersonic Speeds
, 1960 Harriet J. Smith
openalex +1 more source
Some of the next articles are maybe not open access.
Related searches:
Related searches:
2022
The nozzle flow is considered to be much more important in aerospace applications. Based on the pressure, velocity and temperature, flow velocity, Mach number and area, the nozzle shape will vary to meet the required condition. Nozzle is a part where the potential energy is converted into kinetic energy.
Nithya Subramani +3 more
openaire +1 more source
The nozzle flow is considered to be much more important in aerospace applications. Based on the pressure, velocity and temperature, flow velocity, Mach number and area, the nozzle shape will vary to meet the required condition. Nozzle is a part where the potential energy is converted into kinetic energy.
Nithya Subramani +3 more
openaire +1 more source
Progress in Aerospace Sciences, 1974
Abstract This report gives a survey of the inviscid supersonic flow through a straight lattice row. The main subject of this paper is dedicated to the supersonic inlet and outlet flow at such a cascade. It is shown that the cascade flow behaviour is altered radically when the axial velocity component changes from supersonic to subsonic velocities or ...
H.-J. Lichtfuss, H. Starken
openaire +1 more source
Abstract This report gives a survey of the inviscid supersonic flow through a straight lattice row. The main subject of this paper is dedicated to the supersonic inlet and outlet flow at such a cascade. It is shown that the cascade flow behaviour is altered radically when the axial velocity component changes from supersonic to subsonic velocities or ...
H.-J. Lichtfuss, H. Starken
openaire +1 more source