다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기
Applied thermal engineering, v.109 pt.A, 2016년, pp.238 - 250
Xue, X. , Yu, Y.
AI-Helper
Numerical simulations are carried out to investigate the base drag and energy characteristics of a base-bleed projectile with and without containing the effect of a post-combustion process for a boattailed afterbody in a supersonic flow, and then to analyze the key factor of drag reduction and press...
AIAA J. Sahu 23 9 1348 1985 10.2514/3.9091 Navier-Stokes computations of projectile base flow with and without mass injection
J. Spacecraft Rockets Viswanath 27 3 234 1990 10.2514/3.26130 Effectiveness of passive devices for axisymmetric base drag reduction at Mach 2
J. Fluid Mech. Wood 29 2 259 1967 10.1017/S0022112067000795 Visualisation of an Incompressible Wake with Base Bleed
Prog. Astronaut. Aeronaut., AIAA Murthy 40 307 1976 Base combustion effects on base pressure, aerodynamics of base combustion
AIAA J. Mathur 34 34 1153 2012 Velocity and turbulence measurements in a supersonic base flow with mass bleed
Int. J. Therm. Sci. Bournot 45 11 1052 2006 10.1016/j.ijthermalsci.2006.01.018 Improvements of the base bleed effect using reactive particles
J. Appl. Mech. Korst 23 593 1956 10.1115/1.4011405 A theory for base pressures in transonic and supersonic flow
J. Roy. Aeronaut. Soc. Badrinarayanan 65 475 1961 10.1017/S0368393100074927 An experimental investigation of base flows at supersonic speeds
AIAA J. Bowman 5 5 1524 1967 10.2514/3.4245 Cylindrical afterbodies in supersonic flow with gas ejection
AIAA J. Przirembel 8 12 2279 1970 10.2514/3.6104 Turbulent axisymmetric near-wake at Mach four with base injection
Sinha R, Zakkay V, Sinha R, et al., Experimental and Theoretical Investigation of the Near Wake in an Axisymmetric Supersonic Flow with and without Base Injection, AGU Fall Meeting, 1968.
AIAA J. Hubbartt 19 6 745 1981 10.2514/3.50998 Mach 3 hydrogen external/base burning
J. Propul. Power Ding 8 3 630 1992 10.2514/3.23525 Wind tunnel study of aerodynamic characteristics of base combustion
Phys. Fluids Bourdon 15 2 499 2003 10.1063/1.1531995 Visualization of a central bleed jet in an axisymmetric, compressible base flow
AIAA J. Bowman 6 12 2429 1968 10.2514/3.5009 Cylindrical afterbodies at M sub infinity equals 2 with hot gas ejection
Combust. Flame Gross 160 5 982 2013 10.1016/j.combustflame.2013.01.016 Coupling micro and meso-scale combustion models of AP/HTPB propellants
J. Spacecraft Rockets Kaurinkoski 35 5 606 1997 10.2514/2.3392 Numerical simulation of a supersonic base bleed projectile with improved turbulence modelling
Rose 2004 Proceedings of the 21st International Symposium on Ballistics, Adelaide, South Australia, and 19-23 April 2004 Drag reduction through after-burning of base bleed gases
10.2514/6.1991-2077 H.J. Gibeling, R.C. Buggeln, Reacting Flow Models for Navier-Stokes Analysis of Projectile Base Combustion, AIAA/SAE/ASME/ASEE 27th Joint Propulsion Conference, AIAA Paper 91-2077, June 1991.
AIAA J. Hubbartt 19 1502 1981 10.2514/3.60088 External/base burning for base drag reduction at Mach 3
AIAA J. Menter 32 8 1598 1994 10.2514/3.12149 Two equation eddy-viscosity turbulence models for engineering application
AIAA Bardina 1997-2121 1997 Turbulence modeling validation
Vincenti 1965 Introduction to Physical Gas Dynamics
J. Propul. Power Chakravarthy 13 4 471 1997 10.2514/2.5208 Mechanism of burning rate enhancement of composite solid propellants by ferric oxide
Kuo 1994 Fundamentals of Solid-Propellant Combustion
Hoffmann vol. II 2000
J. Ballistics Ding 8 4 79 1996 A study of some parameters influence on performance of drag reduction by base burning
*원문 PDF 파일 및 링크정보가 존재하지 않을 경우 KISTI DDS 시스템에서 제공하는 원문복사서비스를 사용할 수 있습니다.
Copyright KISTI. All Rights Reserved.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.