J.-E. Brune, C. Hofmann, T. Rödiger, L. Jakobs, T. Sander, Ch. Mundt: Transitional High-Enthalpy Boundary-Layer Measurements by ALTP Heat-Flux Sensors. AIAA-2025-2014, AIAA Scitech, 2025.https://doi.org/10.2514/6.2025-2014

S. W. Powers, B. C. Chynoweth, J. S. Jewell, A. Sorensen, J. Romano: Experimentation and Low-Order Modeling of Forward-Facing Cavities at Angles-of-Attack in Mach Six Quiet Flow. AIAA2023-4153. AIAA Aviation Forum, 2024. https://doi.org/10.1063/5.0137927

M. Thele, C. Selcan, T. Sander, T. Rödiger, Ch. Mundt: Bluntness induced boundary layer modes excitation, AIAA Journ. Spacecraft and Rockets, A35127, 2022 https://doi.org/10.2514/1.A35127

V. Wartemann, G.P. Camillo, J. Neumann, A. Weber, A. Wagner: Stability Analyses of Hypersonic, Conical Flows with Transpiration Cooling. IUTAM Bookseries, vol. 38. 2022. https://doi.org/10.1007/978-3-030-67902-6_59

G.P. Camillo, A. Wagner, C. Dittert, L. Benjamin, V. Wartemann, J. Neumann, R: Hink: Experimental investigation of the effect of transpiration cooling on second mode instabilities in a hypersonic boundary layer. Exp Fluids 61, 162, 2020. https://doi.org/10.1007/s00348-020-02994-8

M.A. Kegerise, S.J. Rufer: Unsteady heat-flux measurements of second-mode instability waves in a hypersonic flat-plate boundary layer. Exp Fluids 57, 130, 2016. https://doi.org/10.1007/s00348-016-2214-9

T. Rödiger: Atomic Layer Thermopile (ALTP) – sensors for high-bandwidth, quantitative surface heat-flux measurements. AIAA Aviation Forum: Invited Session on Advanced Measurement Capability Needs for Understanding Hypersonic Laminar-to-Turbulent Transition, 2017.

V. Wartemann, P. G. Camillo, P. Reiter, J. Neumann, A. Wagner: Influence of transpiration cooling on second-mode instabilities investigated on hypersonic, conical flows. CEAS Space J 11, 341–350, 2019. https://doi.org/10.1007/s12567-019-00249-9

A. Wagner: Passive hypersonic boundary layer transition control using ultrasonically absorptive carbon-carbon ceramic with random microstructure. Dissertation, Katholieke Universiteit Leuven, 2014.

E. Marineau, D. Lewis, M. Smith, J. Lafferty, M. White, A. Amar: Investigation of Hypersonic Laminar Heating Augmentation in the Stagnation Region. AIAA2013-0308, AIAA Scitech, 2013. https://doi.org/10.2514/6.2013-308

D. Bountin, T. Chimitov, A.A. Maslov, A. Novikov, I. Egorov, A. Fedorov, S. Utyuzhnikov: Stabilization of a Hypersonic Boundary Layer Using a Wavy Surface, AIAA J., vol. 51, https://doi.org/10.2514/1.J052044

S. Willems, A. Gülhan: Shock Induced Laminar-Turbulent Transition on a Flat Plate at Mach 6. 2013. https://api.semanticscholar.org/CorpusID:43989965

D. Heitmann, T. Rödiger, C. Kähler, H. Knauss, R. Radespiel, S. Wagner: Non-intrusive generation of instability waves in a planar hypersonic boundary layer. Exp Fluids, Vol. 50, 2011. https://doi.org/10.1007/s00348-010-0949-2

T. Rödiger, H. Knauss, M. Estorf, S. Schneider, B.V. Smorodsky: Hypersonic instability waves measured using fast-response heat-flux gauges, AIAA Journal of Spacecraft & Rockets, Vol. 46, No. 2, pp. 266-273, 2009. https://doi.org/10.2514/1.37026

T. Rödiger, H. Knauss, B.V. Smorodsky, D.A. Bountin, A.A. Maslov, D. Heitmann, S. Wagner, E. Krämer, R. Radespiel: Hypersonic instability waves measured on a circular cone using fast-response surface heat-flux and pressure gauges. IUTAM Bookseries, 2009

A.A. Maslov, D.A. Bountin, A. Shiplyuk, Q. Shen, Z. Bi: Experimental study of compressible boundary layer on a cone at angles of attack. Acta Mech Sin 25, 325–333, 2009. https://doi.org/10.1007/s10409-009-0228-8

T. Roediger, H. Knauss, E. Kraemer, B.V. Smorodsky, D.A. Bountin, A.A. Maslov, D. Heitmann: Hypersonic instability waves measured on a flat plate at Mach 6. Proc. ICMAR 2008.

D. Heitmann, T. Roediger, C. Kähler, H. Knauss, R. Radespiel, E. Krämer: Disturbance-level and roughness-induced transition measurements in a conical boundary layer at Mach 6, AIAA-2008-3951, AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2008.

H. Knauss, T. Roediger, J. Srulijes, D.A. Bountin, B.V. Smorodsky, A.A. Maslov: A Novel Sensor for Fast Heat Flux Measurements, AIAA Journal of Spacecraft & Rockets, Vol. 46, No. 2, pp. 255-265, 2009. https://doi.org/10.2514/1.32011

T. Roediger, H. Knauss, M. Estorf, S.P. Schneider, B.V. Smorodsky, E. Kraemer: Hypersonic instability waves measured using fast-response heat-flux gauges; AIAA-2008-0638, 46th AIAA Aerospace Sciences Meeting and Exhibit, 2008.

H. Knauss, T. Roediger, D.A. Bountin, B.V. Smorodsky, J. Srulijes, F. Seiler, A.A: Maslov,U. Gaisbauer, E. Kraemer: A novel sensor for fast heat flux measurements. AIAA-2006-3637, AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 2006.

A.A. Maslov, D.A. Bountin, A.N. Shipyluk, B.V. Smorodsky, H. Knauss, H., U. Gaisbauer, S. Wagner, J. Betz: ALTP sensor application for boundary layer measurements,” Proc. ICMAR, 2004.

A.A. Maslov: Stabilization of Hypersonic Boundary Layer by Microstructural Porous Coating. IUTAM Symposium on One Hundred Years of Boundary Layer Research. Solid mechanics and its applications, vol 129. 2004. https://doi.org/10.1007/978-1-4020-4150-1_33