| Year |
Citation |
Score |
| 2019 |
Hornung HG. Effect of Conical Free Stream on Shock Stand-Off Distance Aiaa Journal. 57: 4115-4116. DOI: 10.2514/1.J058385 |
0.318 |
|
| 2019 |
Hornung HG, Schramm JM, Hannemann K. Hypersonic flow over spherically blunted cone capsules for atmospheric entry. Part 1. The sharp cone and the sphere Journal of Fluid Mechanics. 871: 1097-1116. DOI: 10.1017/Jfm.2019.342 |
0.37 |
|
| 2016 |
Schmidt BE, Bitter NP, Hornung HG, Shepherd JE. Injection into supersonic boundary layers Aiaa Journal. 54: 161-173. DOI: 10.2514/1.J054123 |
0.489 |
|
| 2016 |
Hornung HG. A model problem for a supersonic gas jet from a moon Journal of Fluid Mechanics. 795: 950-971. DOI: 10.1017/Jfm.2016.184 |
0.374 |
|
| 2015 |
Parziale NJ, Shepherd JE, Hornung HG. Observations of hypervelocity boundary-layer instability Journal of Fluid Mechanics. 781: 87-112. DOI: 10.1017/Jfm.2015.489 |
0.501 |
|
| 2014 |
Parziale NJ, Shepherd JE, Hornung HG. Free-stream density perturbations in a reflected-Shock tunnel Experiments in Fluids. 55. DOI: 10.1007/S00348-014-1665-0 |
0.427 |
|
| 2014 |
Schmidt BE, Bitter NP, Hornung HG, Shepherd JE. Experimental investigation of gas injection into the boundary layer on a slender body in supersonic flow Aiaa Aviation 2014 -7th Aiaa Theoretical Fluid Mechanics Conference. |
0.364 |
|
| 2013 |
Parziale NJ, Rabinovitch J, Blanquart G, Hornung HG, Shepherd JE. Proposed vertical expansion tunnel Aiaa Journal. 51: 2792-2799. DOI: 10.2514/1.J052389 |
0.338 |
|
| 2013 |
Parziale NJ, Shepherd JE, Hornung HG. Differential interferometric measurement of instability in a hypervelocity boundary layer Aiaa Journal. 51: 750-753. DOI: 10.2514/1.J052013 |
0.432 |
|
| 2013 |
Parziale NJ, Shepherd JE, Hornung HG. Differential interferometric measurement of instability at two points in a hypervelocity boundary layer 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013. |
0.374 |
|
| 2010 |
Hornung HG. Deriving features of reacting hypersonic flow from gradients at a curved shock Aiaa Journal. 48: 287-296. DOI: 10.2514/1.39993 |
0.344 |
|
| 2010 |
Sanderson SR, Austin JM, Liang Z, Pintgen F, Shepherd JE, Hornung HG. Reactant jetting in unstable detonation Progress in Aerospace Sciences. 46: 116-131. DOI: 10.1016/J.Paerosci.2009.11.002 |
0.334 |
|
| 2010 |
Wen C, Hornung H. Nonequilibrium Recombination after a Curved Shock Wave Progress in Aerospace Sciences. 46: 132-139. DOI: 10.1016/J.Paerosci.2009.11.001 |
0.388 |
|
| 2010 |
Marineau EC, Laurence SJ, Hornung HG. Apollo-shaped capsule boundary layer transition at high-enthalpy in T5 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.701 |
|
| 2009 |
Laurence SJ, Hornung HG. Image-based force and moment measurement in hypersonic facilities Experiments in Fluids. 46: 343-353. DOI: 10.1007/S00348-008-0565-6 |
0.666 |
|
| 2009 |
Leyva IA, Jewell JS, Laurence S, Hornung HG, Shepherd JE. On the impact of injection schemes on transition in hypersonic boundary layers 16th Aiaa/Dlr/Dglr International Space Planes and Hypersonic Systems and Technologies Conference. |
0.691 |
|
| 2009 |
Leyva IA, Laurence S, Beierholm AWK, Hornung HG, Wagnild R, Candler G. Transition delay in hypervelocity boundary layers by means of CO 2/acoustic instability interactions 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. |
0.709 |
|
| 2008 |
Mouton CA, Hornung HG. Experiments on the mechanism of inducing transition between regular and Mach reflection Physics of Fluids. 20. DOI: 10.1063/1.3042261 |
0.404 |
|
| 2008 |
Hornung HG, Pullin DI, Ponchaut NF. On the question of universality of imploding shock waves Acta Mechanica. 201: 31-35. DOI: 10.1007/S00707-008-0070-2 |
0.305 |
|
| 2007 |
Laurence SJ, Deiterding R, Hornung HG. Proximal bodies in hypersonic flow Journal of Fluid Mechanics. 590: 209-237. DOI: 10.1017/S0022112007007987 |
0.685 |
|
| 2006 |
Wright MJ, Olejniczak J, Brown JL, Hornung HG, Edquist KT. Modeling of shock tunnel aeroheating data on the Mars Science Laboratory aeroshell Journal of Thermophysics and Heat Transfer. 20: 641-651. DOI: 10.2514/1.19896 |
0.386 |
|
| 2006 |
Ponchaut NF, Hornung HG, Pullin DI, Mouton CA. On imploding cylindrical and spherical shock waves in a perfect gas Journal of Fluid Mechanics. 560: 103-122. DOI: 10.1017/S0022112006000590 |
0.337 |
|
| 2004 |
El-Naggar MY, Klamo JT, Tan MH, Hornung HG. Experimental verification of the mach-number field in a supersonic Ludwieg tube Aiaa Journal. 42: 1721-1724. DOI: 10.2514/1.3416 |
0.417 |
|
| 2004 |
Sanderson SR, Hornung HG, Sturtevant B. The influence of non-equilibrium dissociation on the flow produced by shock impingement on a blunt body Journal of Fluid Mechanics. 516: 1-37. DOI: 10.1017/S0022112004000357 |
0.349 |
|
| 2003 |
Fujii K, Hornung HG. Experimental investigation of high-enthalpy effects on attachment-line boundary-layer transition Aiaa Journal. 41: 1282-1291. DOI: 10.2514/2.2096 |
0.434 |
|
| 2003 |
Kumar S, Hornung HG, Sturtevant B. Growth of shocked gaseous interfaces in a conical geometry Physics of Fluids. 15: 3194-3208. DOI: 10.1063/1.1608011 |
0.388 |
|
| 2003 |
Sanderson SR, Hornung HG, Sturtevant B. Aspects of planar, oblique and interacting shock waves in an ideal dissociating gas Physics of Fluids. 15: 1638-1649. DOI: 10.1063/1.1572162 |
0.328 |
|
| 2002 |
Rasheed A, Hornung HG, Fedorov AV, Malmuth ND. Experiments on passive hypervelocity boundary-layer control using an ultrasonically absorptive surface Aiaa Journal. 40: 481-489. DOI: 10.2514/2.1671 |
0.69 |
|
| 2002 |
Lemieux P, Hornung H. Development and application of streakline visualization in hypervelocity flows Experiments in Fluids. 33: 188-195. DOI: 10.1007/S00348-002-0433-8 |
0.384 |
|
| 2002 |
Hornung HG. Hypersonic flow over bodies in tandem Shock Waves. 11: 441-445. DOI: 10.1007/S001930200131 |
0.32 |
|
| 2001 |
Fedorov AV, Malmuth ND, Rasheed A, Hornung HG. Stabilization of hypersonic boundary layers by porous coatings Aiaa Journal. 39: 605-610. DOI: 10.2514/2.1382 |
0.691 |
|
| 2001 |
Hornung HG, Lemieux P. Shock layer instability near the Newtonian limit of hypervelocity flows Physics of Fluids. 13: 2394-2402. DOI: 10.1063/1.1383591 |
0.439 |
|
| 2001 |
Hornung HG, Schwendeman DW. Oblique shock reflection from an axis of symmetry: Shock dynamics and relation to the Guderley singularity Journal of Fluid Mechanics. 438: 231-245. DOI: 10.1017/S0022112001004360 |
0.335 |
|
| 2001 |
Fujii K, Hornung HG. An experiment of high enthalpy effect on attachment line transition 15th Aiaa Computational Fluid Dynamics Conference. |
0.347 |
|
| 2001 |
Rasheed A, Hornung HG, Fedorov AV, Malmuth ND. Experiments on passive hypervelocity boundary layer control using a porous surface 39th Aerospace Sciences Meeting and Exhibit. |
0.427 |
|
| 2000 |
Schlamp S, Hornung HG, Sobota TH, Cummings EB. Accuracy and uncertainty of single-shot, nonresonant laser-induced thermal acoustics. Applied Optics. 39: 5477-81. PMID 18354543 DOI: 10.1364/Ao.39.005477 |
0.717 |
|
| 2000 |
Sudani N, Valiferdowsi B, Hornung HG. Test time increase by delaying driver gas contamination for reflected shock tunnels Aiaa Journal. 38: 1497-1503. DOI: 10.2514/2.1138 |
0.302 |
|
| 2000 |
Schlamp S, Hornung HG, Cummings EB. Neural network data analysis for laser-induced thermal acoustics Measurement Science and Technology. 11: 784-794. DOI: 10.1088/0957-0233/11/6/323 |
0.693 |
|
| 2000 |
Hornung HG. Oblique shock reflection from an axis of symmetry Journal of Fluid Mechanics. 409: 1-12. DOI: 10.1017/S0022112099007831 |
0.326 |
|
| 2000 |
Hornung HG. Features of the density field of dissociating hypersonic flows Zamm Zeitschrift Fur Angewandte Mathematik Und Mechanik. 80: 755-763. DOI: 10.1002/1521-4001(200011)80:11/12<755::Aid-Zamm755>3.0.Co;2-5 |
0.337 |
|
| 1999 |
Schlamp S, Cummings EB, Hornung HG. Beam misalignments and fluid velocities in laser-induced thermal acoustics. Applied Optics. 38: 5724-33. PMID 18324083 DOI: 10.1364/Ao.38.005724 |
0.714 |
|
| 1999 |
Olejniczak J, Candler GV, Wright MJ, Leyva I, Hornung HG. Experimental and Computational Study of High Enthalpy Double-Wedge Flows Journal of Thermophysics and Heat Transfer. 13: 431-440. DOI: 10.2514/2.6481 |
0.335 |
|
| 1998 |
Sudani N, Hornung HG. Gasdynamical detectors of driver gas contamination in a high-enthalpy shock tunnel Aiaa Journal. 36: 313-319. DOI: 10.2514/2.383 |
0.349 |
|
| 1998 |
Sudani N, Hornung HG. Stability and analogy of shock wave reflection in steady flow Shock Waves. 8: 367-374. DOI: 10.1007/S001930050129 |
0.431 |
|
| 1998 |
Hornung HG. Gradients at a curved shock in reacting flow Shock Waves. 8: 11-21. DOI: 10.1007/S001930050094 |
0.37 |
|
| 1997 |
Adam PH, Hornung HG. Enthalpy effects on hypervelocity boundary-layer transition: Ground test and flight data Journal of Spacecraft and Rockets. 34: 614-619. DOI: 10.2514/2.3278 |
0.482 |
|
| 1997 |
Germain PD, Hornung HG. Transition on a slender cone in hypervelocity flow Experiments in Fluids. 22: 183-190. DOI: 10.1007/S003480050036 |
0.437 |
|
| 1997 |
Hornung HG. Technical note On the stability of steady–flow regular and Mach reflection Shock Waves. 7: 123-125. DOI: 10.1007/S001930050068 |
0.306 |
|
| 1997 |
Adam PH, Hornung HG. Enthalpy effects on hypervelocity boundary layer transition: Experiments and free flight data 35th Aerospace Sciences Meeting and Exhibit. |
0.381 |
|
| 1996 |
Bélanger J, Hornung HG. Transverse jet mixing and combustion experiments in hypervelocity flows Journal of Propulsion and Power. 12: 186-192. DOI: 10.2514/3.24009 |
0.366 |
|
| 1995 |
Cummings EB, Leyva IA, Hornung HG. Laser-induced thermal acoustics (LITA) signals from finite beams. Applied Optics. 34: 3290-302. PMID 21052135 DOI: 10.1364/Ao.34.003290 |
0.345 |
|
| 1995 |
Cummings EB, Hornung HG, Brown MS, Debarber PA. Measurement of gas-phase sound speed and thermal diffusivity over a broad pressure range using laser-induced thermal acoustics. Optics Letters. 20: 1577-9. PMID 19862088 DOI: 10.1364/Ol.20.001577 |
0.352 |
|
| 1995 |
Wen CY, Hornung HG. Non-equilibrium dissociating flow over spheres Journal of Fluid Mechanics. 299: 389-405. DOI: 10.1017/S0022112095003545 |
0.364 |
|
| 1995 |
Hornung HG, Turner S, Willert C. The flow field downstream of a hydraulic jump Journal of Fluid Mechanics. 287: 299-316. DOI: 10.1017/S0022112095000966 |
0.38 |
|
| 1994 |
Bridges DH, Hornung HG. Elliptic tip effects on the vortex wake of an axisymmetric body at incidence Aiaa Journal. 32: 1437-1445. DOI: 10.2514/3.12213 |
0.305 |
|
| 1993 |
Rock SG, Candler GV, Hornung HG. Analysis of thermochemical nonequilibrium models for carbon dioxide flows Aiaa Journal. 31: 2255-2262. DOI: 10.2514/3.11923 |
0.318 |
|
| 1989 |
Ludwieg H, Hornung H. The instability of a liquid film on a wall exposed to an air flow Journal of Fluid Mechanics. 200: 217-233. DOI: 10.1017/S0022112089000637 |
0.357 |
|
| 1986 |
Hornung H. Regular and Mach Reflection of Shock Waves Annual Review of Fluid Mechanics. 18: 33-58. DOI: 10.1146/Annurev.Fl.18.010186.000341 |
0.328 |
|
| 1982 |
Hornung HG, Robinson ML. Transition from regular to Mach reflection of shock waves Part 2. The steady-flow criterion Journal of Fluid Mechanics. 123: 155-164. DOI: 10.1017/S0022112082003000 |
0.392 |
|
| 1982 |
Hornung HG, Taylor JR. Transition from regular to Mach reflection of shock waves Part 1. The effect of viscosity in the pseudosteady case Journal of Fluid Mechanics. 123: 143-153. DOI: 10.1017/S0022112082002997 |
0.381 |
|
| 1980 |
Hornung HG, Houwing AFP. Shock detachment from cones in a relaxing gas Journal of Fluid Mechanics. 101: 307-319. DOI: 10.1017/S002211208000167X |
0.353 |
|
| 1979 |
Hornung HG, Oertel H, Sandeman RJ. Transition to Mach reflexion of shock waves in steady and pseudosteady flow with and without relaxation Journal of Fluid Mechanics. 90: 541-560. DOI: 10.1017/S002211207900238X |
0.452 |
|
| 1979 |
Hornung HG, Smith GH. The influence of relaxation on shock detachment Journal of Fluid Mechanics. 93: 225-239. DOI: 10.1017/S0022112079001865 |
0.381 |
|
| 1976 |
Hornung HG, Killen P. A stationary oblique breaking wave for laboratory testing of surfboards Journal of Fluid Mechanics. 78: 459-480. DOI: 10.1017/S0022112076002553 |
0.358 |
|
| 1976 |
Hornung HG. Non-equilibrium ideal-gas dissociation after a curved shock wave Journal of Fluid Mechanics. 74: 143-159. DOI: 10.1017/S0022112076001730 |
0.404 |
|
| 1975 |
Ebrahim NA, Hornung HG. HIGH-ENTHALPY NONEQUILIBRIUM CARBON DIOXIDE NOZZLE AND WEDGE FLOWS: EXPERIMENT AND CALCULATIONS Aiaa Journal. 13: 845-846. DOI: 10.2514/3.60456 |
0.347 |
|
| 1974 |
Kewley DJ, Hornung HG. Non-equilibrium dissociating nitrogen flow over a wedge Journal of Fluid Mechanics. 64: 725-736. DOI: 10.1017/S002211207400187X |
0.372 |
|
| 1972 |
Hornung HG. Non-equilibrium dissociating nitrogen flow over spheres and circular cylinders Journal of Fluid Mechanics. 53: 149-176. DOI: 10.1017/S0022112072000084 |
0.346 |
|
| 1971 |
Hornung HG. Nonequilibrium dissociating nitrogen flow over a circular cylinder Aiaa Journal. 9: 1198-1200. DOI: 10.2514/3.6338 |
0.302 |
|
| 1970 |
HORNUNG HG, MCINTOSH MK. Prevention of flare-induced separation by boundary-layer bleed Aiaa Journal. 8: 1156-1157. DOI: 10.2514/3.5854 |
0.394 |
|
| 1969 |
Hornung HG. Some aspects of hypersonic flow over power law bodies Journal of Fluid Mechanics. 39: 143-162. DOI: 10.1017/S0022112069002084 |
0.399 |
|
| 1963 |
Hornung HG, Joubert PN. The mean velocity profile in three-dimensional turbulent oundary layers Journal of Fluid Mechanics. 15: 368-384. DOI: 10.1017/S0022112063000318 |
0.334 |
|
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