SCOPUS 정보 검색 플랫폼

Journal of Spacecraft and Rockets

Volumn 38, Issue 6, 2001, Pages 820-827

Computational fluid dynamics prediction of Hyper-X Stage separation aerodynamics

(4) Buning, Pieter G a,c Wong, Tin Chee b,d Dilley, Arthur D b,e Pao, Jenn L b,f

a NASA LANGLEY RESEARCH CENTER (United States)

b FDC/NYMA (United States)

c AIAA (United States)

d US Army Aviation and Missile Command Redstone Arsenal (United States)

e RAYTHEON COMPANY (United States)

f NORTHROP GRUMMAN CORPORATION (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOOSTERS (ROCKET); COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; DATABASE SYSTEMS; EXTRAPOLATION; FLIGHT DYNAMICS; HYPERSONIC AERODYNAMICS; WIND TUNNELS;

AERODYNAMIC DATABASE EXTRAPOLATION; FLIGHT TEST; HYPER X STAGE SEPARATION AERODYNAMICS; PEGASUS LAUNCH VEHICLE;

RESEARCH AIRCRAFT;

EID: 0035518409 PISSN: 00224650 EISSN: None Source Type: Journal
DOI: 10.2514/2.3771 Document Type: Article

Times cited : (33)

References (27)

1
- 85085845996
- AIAA Paper 99-4818, Nov
- (1999) Hyper-X Stage Separation-Background and Status
- Reubush, D.E.¹

2
- 0035518652
- Hyper-X stage separation wind-tunnel test program
- (2001) Journal of Spacecraft and Rockets , vol.38 , Issue.6 , pp. 811-819
- Woods, W.C.¹ Holland, S.D.² DiFulvio, M.³

3
- 0007826669
- Hyper-X Program Office, HX-432, TN 99-289, NASA Langley Research Center, Hampton, VA, March
- (2000) Pre-Test SAMcfd Euler Analysis for Hyper-X Stage Separation AEDC Tests
- Pao, J.L.¹

4
- 0035518190
- Aerodynamic database development for the Hyper-X airframe-integrated scramjet propulsion experiments
- (2001) Journal of Spacecraft and Rockets , vol.38 , Issue.6 , pp. 803-810
- Engelund, W.C.¹ Holland, S.D.² Cockrell, C.E.³ Bittner, R.D.⁴

5
- 0035518636
- Integrated aeropropulsive computational fluid dynamics methodology for the Hyper-X flight experiment
- (2001) Journal of Spacecraft and Rockets , vol.38 , Issue.6 , pp. 836-843
- Cockrell, C.E.¹ Engelund, W.C.² Bittner, R.D.³ Jentink, T.N.⁴ Dilley, A.D.⁵ Frendi, A.⁶

6
- 0000912464
- Three-dimensional fluid-structure interaction using a finite element solver and adaptive remeshing
- (1990) Computing Systems in Engineering , vol.1 , Issue.2-4 , pp. 257-272
- Lohner, R.¹

7
- 0007822578
- ResearchSouth Inc., Phase III Final Rept., NASA SBIR NAS1-97106, Huntsville, AL, Feb
- (1998) Data Transfer Between SAMcfd and NASTRAN
- Spradley, L.W.¹

8
- 0004229817
- AIAA Paper 97-0644, Jan
- (1997) Recent Enhancements to OVERFLOW
- Jespersen, D.C.¹ Pulliam, T.H.² Buning, P.G.³

9
- 0003798134
- NASA Langley Research Center, Hampton, VA, Jan
- (2000) OVERFLOW User's Manual, Version 1.8m
- Buning, P.G.¹ Jespersen, D.C.² Pulliam, T.H.³ Klopfer, G.H.⁴ Chan, W.M.⁵ Slotnick, J.P.⁶ Krist, S.E.⁷ Renze, K.J.⁸

10
- 0007823699
- AIAA Paper 99-3303, June
- (1999) Advances in Automatic Overset Grid Generation Around Surface Discontinuities
- Chan, W.M.¹ Gomez, R.J.²

11
- 84983167466
- Arnold Engineering Development Center, AEDC-TR-91-8, Arnold AFB, TN, Nov
- (1991) PEGSUS 4.0 User's Manual
- Suhs, N.E.¹ Tramel, R.W.²

12
- 0004108629
- McGraw-Hill, New York
- (1974) Viscous Fluid Flow , pp. 498
- White, F.M.¹

13
- 0007823324
- Free-flight measurements of turbulent boundary layer skin friction in the presence of severe aerodynamic heating at mach numbers from 2.8 to 7.0
- (1956) Journal of the Aeronautical Sciences , vol.23 , Issue.6 , pp. 536-542
- Sommer, S.C.¹ Short, B.J.²

14
- 0027988926
- A one-equation turbulence model for aerodynamic flows
- (1994) La Recherche Aerospatiale , Issue.1 , pp. 5-21
- Spalart, P.R.¹ Allmaras, S.R.²

15
- 0004002892
- Hermosa Publishers, Albuquerque, NM
- (1998) Verification and Validation in Computational Science and Engineering , pp. 107-141
- Roache, P.J.¹

16
- 0035518187
- Hyper-X research vehicle experimental aerodynamics test program overview
- (2001) Journal of Spacecraft and Rockets , vol.38 , Issue.6 , pp. 828-835
- Holland, S.D.¹ Woods, W.C.² Engelund, W.C.³

17
- 0007723863
- Hyper-X Program Office, HX-432, TN 98-204, NASA Langley Research Center, Hampton, VA, June
- (1998) Mach 7 Time Accurate, Inviscid Computations with a Fixed 2D Cavity
- Dilley, A.D.¹ Pao, J.L.²

18
- 0003595356
- NASA TM-1998-208444, June
- (1998) CFL3D User's Manual (Version 5.0)
- Krist, S.L.¹ Biedron, R.T.² Rumsey, C.L.³

19
- 0007773143
- Hyper-X Program Office, HX-432, TN 00-313, NASA Langley Research Center, Hampton, VA, May
- (2000) Two-Dimensional, Time-Accurate, Viscous Analysis with a Fixed Cavity Geometry
- Wong, T.-C.¹

20
- 0007773145
- AIAA Paper 99-3302, June
- (1999) Unsteady Aerodynamic Simulation of Static and Moving Bodies Using Scalable Computers
- Meakin, R.¹ Wissink, A.²

21
- 0002045158
- The chimera method of simulation for unsteady for unsteady three-dimensional viscous flow
- edited by M. Hafez and K. Oshima, Wiley, New York
- (1995) Computational Fluid Dynamics Review 1995 , pp. 70-86
- Meakin, R.¹

22
- 85006868075
- AIAA Paper 89-1996, June
- (1989) Unsteady Aerodynamic Simulation of Multiple Bodies in Relative Motion
- Meakin, R.¹ Suhs, N.²

23
- 85086949045
- AIAA Paper 99-4807, Nov
- (1999) Computational Simulation of Hypersonic Vehicle Separation from Its Booster
- Luo, X.¹ Baysal, O.²

24
- 0007723864
- AIAA Paper 99-3412, June
- (1999) Unsteady Separation of a Two-Stage Hypersonic Vehicle
- Cvrlje, T.¹

25
- 0007772005
- Hyper-X Program Office, HX-241, NASA Langley Research Center, Hampton, VA, April
- (1997) Hyper-X Aerodynamics and Propulsion Reference Systems
- Roettker, W.A.¹

26
- 0007722965
- Hyper-X Program Office, HX-432, TN 99-249, NASA Langley Research Center, Hampton, VA, Jan
- (2000) Interference Effects of the Fixed Jaw Adapter on the Hyper-X Research Vehicle Aerodynamics
- Pao, J.L.¹

27
- 0007722635
- Hyper-X Program Office, HX-432, TN-00-293, NASA Langley Research Center, Hampton, VA, May
- (2000) Blade Interference Effects on the Hyper-X Research Vehicle Aerodynamics
- Pao, J.L.¹

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.