Box 1
Contains 22 Results:
Edward W. Perkins, Forrest E. Gowen, and Leland H. Jorgensen, "Aerodynamic Characteristics of the NACA RM-10 Research Missile in the Ames 1- by 3-Foot Supersonic Wind Tunnel No. 2. Pressure and Force Measurements at Mach Number of 1.52 and 1.98", 1951
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.
Edward W. Perkins and Leland H. Jorgensen, "Investigations fo the Drag of Various Axially Symmetric Nose Shapes of Fineness Ratio 3 for Mach Numbers From 1.24 to 3.67", 1952
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.
"Correlation by the Hypersonic Similarity Rule of Pressure Distributions and Wave Drags from Minimum-Drag Nose Shapes at Zero Angle of Attack", 1953
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.
Edward W. Perkins and Leland H. Jorgensen, "Comparison of Experimental and Theoretical Normal-Force Distributions (Including Reynolds Number Effects) on an Ogive-Cylinder Body at Mach Number 1.98", 1954
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.
Leland H. Jorgensen and Edward W. Perkins, "Investigation of Some Wake Vortex Characteristics of an Inclined Ogive-Cylinder Body at Mach Number 1.98", 1955
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.
Edward W. Perkins and Leland H. Jorgensen, "Comparison of Experimental and Theoretical Normal-Force Distributions (Including Reynolds Number Effects) on an Ogive-Cylinder Body at Mach Number 1.98", 1956
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.
Elliot D. Katzen and Leland H. Jorgensen, "Aerodynamics of Missiles Employing Wings of Very Low Aspect Ratio at Sumersonic Speeds", 1956
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.
Leland H. Jorgensen and Elliot D. Katzen, "Wing-Body Combinations With Wings of Very Low Aspect Ratio at Sumersonic Speeds", 1956
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.
"Elliptic Cones Alone and With Wings at Supersonic Speeds", 1957
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.
"Experimental Lift-Drag Ratios for Two Families of Wing-Body Combinations at Supersonic Speeds", 1958
The Leland H. Jorgensen papers consist of aerodynamic research reports written by Jorgensen and others. Included is a copy of his dissertation along with conference proceedings for the Advisory Group for Aerospace Research and Development.