Results 241 to 250 of about 14,137 (299)
The Effect of the Chamber-Filling Ratio in Vibratory Shot Peening on Selected Surface Layer Properties of 30HGSA. [PDF]
Materials (Basel)Skoczylas A, Zaleski K.
europepmc +1 more source
Cellular response in three-dimensional spheroids and tissues exposed to real and simulated microgravity: a narrative review. [PDF]
NPJ Microgravityvan den Nieuwenhof DWA +3 more
europepmc +1 more source
Long-Duration Dynamic Numerical Simulation of Combustion and Flow in Hybrid Rocket Motors Considering Nozzle Erosion [PDF]
Xiangyu Meng +5 more
openalex +1 more source
Ceramic Matrix Composite Cyclic Ablation Behavior under Oxyacetylene Torch. [PDF]
Materials (Basel)Ge H, Chen X, Li G, Zhang L.
europepmc +1 more source
Experimental Analysis of the Mechanical Properties of Carbon Foams Under Quasi-Static Compressive Loads. [PDF]
Materials (Basel)Wacławiak K +3 more
europepmc +1 more source
Scaling of Rocket Nozzle Admittances [PDF]
AIAA Journal, 1974 To apply the admittance data measured experimentally for small-scale nozzles, the necessary scaling criteria must be established. The results of an investigation undertaken to determine these criteria are presented and the data indicate that under cold-flow conditions the damping of axial instabilities provided by full-scale nozzles can be determined ...
B. A. Janardan +2 more
openaire +2 more sources
Some of the next articles are maybe not open access.
Related searches:
Related searches:
Journal of Propulsion and Power, 1998
Several nozzle concepts that promise a gain in performance over existing conventional nozzles are discussed in this paper. It is shown that signie cant performance gains result from the adaptation of the exhaust e ow to the ambient pressure. Special attention is then given to altitude-adaptive nozzle concepts, which have recently received new interest ...
Hagemann, G. +3 more
openaire +4 more sources
Several nozzle concepts that promise a gain in performance over existing conventional nozzles are discussed in this paper. It is shown that signie cant performance gains result from the adaptation of the exhaust e ow to the ambient pressure. Special attention is then given to altitude-adaptive nozzle concepts, which have recently received new interest ...
Hagemann, G. +3 more
openaire +4 more sources
Fluid flow in rocket nozzles [PDF]
34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 1998 An analysis is presented to simulate the turbulent compressible flow in converging diverging nozzles using a time-marching finite difference scheme of MacCormack. The Navier-Stokes equations governing the physical domain are transformed to a rectangular computational domain and the resulting equations are cast into finite difference form. The effect of
K. Shukla, V. Jones
openaire +1 more source