Research and design for lifting reentry
- 31 December 1979
- journal article
- review article
- Published by Elsevier in Progress in Aerospace Sciences
- Vol. 19, 1-80
- https://doi.org/10.1016/0376-0421(79)90001-0
Abstract
No abstract availableThis publication has 41 references indexed in Scilit:
- Oscillating delta wings with attached shock wavesAIAA Journal, 1977
- Unsteady hypersonic flow over delta wings with detached shock wavesAIAA Journal, 1976
- Propulsion Options for the Hypersonic Research AirplaneJournal of Aircraft, 1975
- Methods for calculating nonlinear flows with attached shock waves over conical wings.AIAA Journal, 1973
- Experimental study of a high lift re-entry vehicle configuration.AIAA Journal, 1973
- Lee-side vortices on delta wings at hypersonic speeds.AIAA Journal, 1972
- Lift and drag of a wing-cone configuration in hypersonic flowAIAA Journal, 1971
- Stability of oscillating wedges and caret wings in hypersonic and supersonic flows.AIAA Journal, 1969
- NUMERICAL SOLUTION OF THE PROBLEM OF SUPERSONIC FLOW PAST THE LOWER SURFACE OF A DELTA WINGAIAA Journal, 1963
- LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORYAIAA Journal, 1963