Zobrazeno 1 - 10
of 17
pro vyhledávání: '"Gary D. Kuhn"'
Autor:
Michael R. Mendenhall, Marnix F. E. Dillenius, Steven C. Caruso, Gary D. Kuhn, Daniel J. Lesieutre
Publikováno v:
Journal of Spacecraft and Rockets. 31:1007-1015
Pegasus™, a three-stage, air-launched, winged space booster, was developed to provide fast and efficient commercial launch services for small satellites. The aerodynamic design and analysis of the vehicle were conducted without wind-tunnel and subs
Autor:
Gary D. Kuhn
Publikováno v:
31st Aerospace Sciences Meeting.
Autor:
Marnix F. E. Dillenius, Steven C. Caruso, Gary D. Kuhn, Daniel J. Lesieutre, Michael R. Mendenhall
Publikováno v:
29th Aerospace Sciences Meeting.
Publikováno v:
21st Fluid Dynamics, Plasma Dynamics and Lasers Conference.
This report describes the results of research into the interactions between shock waves and turbulent flows using numerical simulations. The research was conducted at transonic speeds with a normal shock wave and two dimensional turbulence, making us
Publikováno v:
28th Aerospace Sciences Meeting.
The objective of the work is to identify the flow mechanism that cause the decrease in spreading rate of supersonic mixing layers as the convective Mach number increases and to suggest means of enhancing the mixing. Two approaches have been taken, on
Autor:
Gary D. Kuhn
Publikováno v:
28th Aerospace Sciences Meeting.
Turbulent flows subjected to oscillations of the mean flow were simulated using a large-eddy simulation computer code for flow in a channel. The objective of the simulations was to provide better understanding of the effects of time-dependent disturb
Autor:
Gary D. Kuhn, Dean R. Chapman
Publikováno v:
Journal of Fluid Mechanics. 170:265-292
Three different Navier-Stokes computational models of incompressible viscoussublayer turbulence have been developed. Comparison of computed turbulence quantities with experiment is made for the mean streamwise velocity, Reynolds stress, correlation c
Calculation of separated turbulent flows on axisymmetric afterbodies including exhaust plume effects
Autor:
Gary D. Kuhn
Publikováno v:
17th Aerospace Sciences Meeting.
A calculative method is presented for turbulent boundary-layer, inviscid flow interactions for axisymmetric configurations of the type used for isolated nozzle afterbody models. The method is applicable to flows with subsonic freestreams, including s
Publikováno v:
25th AIAA Aerospace Sciences Meeting.
Autor:
Jack N. Nielsen, Gary D. Kuhn
Publikováno v:
10th Aerospace Sciences Meeting.
The effects of turbulent mixing and buoyancy on the motion and persistency of a trailing vortex wake behind an aircraft are considered. A model for the characteristics of a turbulent vortex, based on an analogy to a turbulent boundary layer, is prese