Box 13
Contains 152 Results:
Leadon, Bernard M. "Mass in a Turbulent Boundary Layer"
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.
Leadon, Bernard M. "Transpiration Cooling Experiments in a Turbulent Boundary at M = 3", 1956-08
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.
Lange, A. H. "Measurements of Boundary-Layer Transition on a Standard Model to Determine the Relative Disturbance Level in Two Supersonic Wind Tunnels", 1953-02-19
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.
Lange, A. H. "Pressure and Temperature Measurements of the Flow Produced by a 12 X 12 cm Grating Nozzle", 1953-01-28
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.
R. Ladenburg "Interferometric Studies of Faster Sound Phenomena Part II. Analysis of Supersonic Air Jets", 1949-09-01
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.
R. Ladenburg "Optical Studies of Boundary Layer Phenomena on a Flat Plate at Mach Number 2.35", 1952-12-15
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.
Landahl, Marten T. "Unsteady Flow Around Thin Wings at High Mach Numbers", 1955-06
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.
Landon, Stephen A. "Calculation of Three-Body Ionic Recombination Rate", 1967-07-17
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.
Lane, Frank & Zeiberg, Seymour L. "Comments on "Fluctuations in an Equilibrium Turbulent Plasma"", 1964-09-28
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.
Langworhty, Robert A. "The Design and Calibration of a Total Temperature Probe for use in a Mach 5 Turbulent Boundary Layer with Heat Transfer", 1962-06
Subjects covered within this collection include wind tunnel testing, early German rocket science history, and UAH Research Institute history.