1. Brewer, E.B., Craven, C.E.: Experimental Investigation of Base Flow Field at High Altitude for a Four-Engine Clustered Nozzle Configuration. NASA TN D-5164, Washington (1969)
2. Gruhn, P., Henckels, A.: Simulation of a SERN/Afterbody Flow Field regarding heated Nozzle Flow in Hypersonic Facility H2K. In: Breitsamter, C., Laschka, B., et al. (eds.) Notes on Numerical Fluid Mechanics, vol. 78, pp. 236–243. Springer, Heidelberg (2004)
3. Henckels, A., Gruhn, P.: Experimental Studies of Viscous Interaction Effects in Hypersonic Inlets and Nozzle Flow Fields. In: Jacob, D., Sachs, G., Wagner, S. (eds.) Basic Research Technologies for Two-Stage-to-Orbit Vehicles, pp. 383–403. Wiley-VCH, Weinheim (2005)
4. Henckels, A., Gruhn, P., Gülhan, A.: First Experimental Results on the Nozzle/Base Flow Interaction for Launcher Configurations. In: 6th Intern. Symp. on Launcher Technologies, Munich (2005)
5. Herbertz, A., Sippel, M.: Vorbereitung der Untersuchungen zur Heckströmung und Plume-Entwicklung bei Raumtransportsystemen. DLR-IB 647-2004/04, Köln (2005)