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joseph h ruf
joseph h ruf
Verified email at nasa.gov
Title
Cited by
Cited by
Year
The plume physics behind aerospike nozzle altitude compensation and slipstream effect
J Ruf, P McConaughey, J Ruf, P McConaughey
33rd Joint Propulsion Conference and Exhibit, 3218, 1997
901997
Wall pressure unsteadiness and side loads in overexpanded rocket nozzles
WJ Baars, CE Tinney, JH Ruf, AM Brown, DM McDaniels
AIAA journal 50 (1), 61-73, 2012
572012
Nozzle side load testing and analysis at MSFC
J Ruf, D McDaniels, A Brown
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4856, 2009
392009
Characterization of side load phenomena using measurement of fluid/structure interaction
A Brown, R Keanini, J Ruf, D Reed, M D'Agostino
38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 3999, 2002
362002
Computational and experimental study of nozzle performance for rotating detonation rocket engines
AJ Harroun, SD Heister, JH Ruf
Journal of Propulsion and Power 37 (5), 660-673, 2021
322021
A numerical analysis of a three dimensional aerospike
J Ruf, P McConaughey, J Ruf, P McConaughey
33rd Joint Propulsion Conference and Exhibit, 3217, 1997
311997
Details of side load test data and analysis for a truncated ideal contour nozzle and a parabolic contour nozzle
J Ruf, D McDaniels, A Brown
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 6813, 2010
302010
Fully coupled fluid-structure interaction simulations of rocket engine side loads
E Blades, E Luke, J Ruf
48th AIAA/ASME/SAE/ASEE joint propulsion conference & exhibit, 3969, 2012
292012
Sound produced by large area-ratio nozzles during fixed and transient operations
BW Donald, WJ Baars, CE Tinney, JH Ruf
AIAA journal 52 (7), 1474-1485, 2014
242014
Non-stationary shock motion unsteadiness in an axisymmetric geometry with pressure gradient
WJ Baars, JH Ruf, CE Tinney
Experiments in Fluids 56, 1-18, 2015
202015
Plug nozzles-assessment of prediction methods for flow features and engine performance
R Schwane, G Hagemann, P Reijasse
40th AIAA Aerospace Sciences Meeting & Exhibit, 585, 2002
192002
Effect of Aerospike Plug Nozzle Design on Rotating Detonation Engine Performance for Rocket Applications
A Harroun, SD Heister, SV Sardeshmukh, JH Ruf
AIAA Scitech 2019 Forum, 0197, 2019
162019
Flow separation side loads excitation of rocket nozzle FEM
K Smalley, A Brown, J Ruf, J Gilbert
48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2007
142007
Benchmark of FDNS CFD code for direct connect RBCC test data
J Ruf
36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 3726, 2000
132000
Validation of supersonic film cooling modeling for liquid rocket nozzle applications
C Morris, J Ruf
46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 6657, 2010
122010
Measurements of film cooling performance in supersonic environments
D Maqbool, MD Collett, K Dellimore, JH Ruf, CP Cadou
52nd Aerospace Sciences Meeting, 0701, 2014
102014
Computational insight to experimentally observed change in mixing characteristics of an RBCC engine in ejector mode
J West, J Ruf, J Cramer, S Pal, R Santoro
37th Joint Propulsion Conference and Exhibit, 3459, 2001
102001
Time-frequency analysis of rocket nozzle wall pressures during start-up transients
WJ Baars, CE Tinney, JH Ruf
Journal of Physics: Conference Series 318 (9), 092001, 2011
92011
Recovering aerodynamic side loads on rocket nozzles using quasi-static strain-gage measurements
A Brown, J Ruf, D McDaniels
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2009
92009
Experimental results for an annular aerospike with differential throttling
JH Ruf, DM McDaniels
Fifth International Symposium on Liquid Space Propulsion, 2005
72005
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Articles 1–20