Results 131 to 140 of about 385,605 (249)

Film cooling performance analysis of different multi-row cooling hole configurations. [PDF]

Sci Rep
Singh DP, Mom V, Reddy SR.
europepmc   +1 more source

Modelling of heat addition to near-critical and supercritical fluids. [PDF]

Sci Rep
Lamanna G, Steinhausen C.
europepmc   +1 more source

Aerodynamics of Mars entry probe-lander configurations at a Mach number of 10

, 1970
Robert I Sammonds
openalex   +1 more source

Low Mach number limit of the full Navier-Stokes equations

, 2005
Thomas Alazard
openalex   +2 more sources

Investigation of ion acoustic double layers in magnetized plasma with two nonextensive electron species. [PDF]

Sci Rep
Hatami MM.
europepmc   +1 more source

Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable-sweep Wings

, 1960
Gerald V. Foster, O. A. Morris
openalex   +1 more source

Application of a Total Pressure Sensor in Supersonic Flow for Shock Wave Analysis Under Low-Pressure Conditions. [PDF]

Sensors (Basel)
Bílek M, Maxa J, Šabacká P, Bayer R, Binar T, Bača P, Votava J, Tobiáš M, Žák M.   +8 more
europepmc   +1 more source

Bow shock oscillations of Mars under weakly disturbed solar wind conditions. [PDF]

Nat Commun
Cheng L, Wang Y, Ma Y, Lillis R, Halekas J, Langlais B, Zhang T, Zhang A, Wang G, Xiao S, Zou Z, Chi Y, Hao X, Li Y, Pan Z, Liu K.   +15 more
europepmc   +1 more source

Mach number dependence of the onset of dynamo action [PDF]

, 2004
Nils Erland L. Haugen, Axel Brandenburg, A. J. Mee   +2 more
openalex   +1 more source

Application of deep reinforcement learning for aerodynamic control around an angled airfoil via synthetic jet. [PDF]

Sci Rep
Hammouda NG, Khan R, Mostafa L, Musa VA, Rajab H, Singh NSS, Aich W, Hajlaoui K.   +7 more
europepmc   +1 more source