CaltechTHESIS
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Jump to: B | C | F | G | L | M | P | W
Number of items: 14.

B

Benezra, Joseph Nissim (1949) Supersonic Flow in a Two-Dimensional Asymmetric Channel. Engineer's thesis, California Institute of Technology. doi:10.7907/GYFS-PN59. https://resolver.caltech.edu/CaltechETD:etd-02102009-091251

Bevernick, Richard Alexander (1949) The Effect of Reynolds Number on the Flow Field About a 70° Cone. Engineer's thesis, California Institute of Technology. doi:10.7907/FGSF-5183. https://resolver.caltech.edu/CaltechETD:etd-01232009-104850

Bottenberg, William Robert (1949) Effect of Reynolds Number on the Flow About a Finite Cone of 70 Degrees. Engineer's thesis, California Institute of Technology. doi:10.7907/PPKS-C120. https://resolver.caltech.edu/CaltechETD:etd-01222009-153637

C

Chase, Patrick Stanley (1950) Flexible Plate Supersonic Wind Tunnel Flow Correction to Account for Plate Elastic Properties. Engineer's thesis, California Institute of Technology. doi:10.7907/EC0T-P917. https://resolver.caltech.edu/CaltechETD:etd-02242009-093505

F

Fossier, Mike Walter and Small, John (1947) Supersonic Wind Tunnel Tests of Two Rocket Propelled Projectile Models. Engineer's thesis, California Institute of Technology. doi:10.7907/71EK-W641. https://resolver.caltech.edu/CaltechETD:etd-12092008-082853

G

Gompf, George Edward (1949) Supersonic Nozzle Design for Viscous Fluids. Engineer's thesis, California Institute of Technology. doi:10.7907/R422-S076. https://resolver.caltech.edu/CaltechETD:etd-01262009-141501

L

Leydon, John Koebig and Miller, Walter Bernard (1945) An Investigation of Wind Tunnel Wall Effects at High Mach Numbers. Engineer's thesis, California Institute of Technology. doi:10.7907/HNBB-CK44. https://resolver.caltech.edu/CaltechTHESIS:10162015-093151774

M

MacKinnon, Neil Allan (1949) Flow Field Around a Finite Cone with Shock. Engineer's thesis, California Institute of Technology. doi:10.7907/XR4M-9R51. https://resolver.caltech.edu/CaltechETD:etd-02182009-110248

Muirhead, Vincent Uriel (1949) Flow Field Around a Finite Cone with Shock. Engineer's thesis, California Institute of Technology. doi:10.7907/7GMA-0V07. https://resolver.caltech.edu/CaltechETD:etd-01282009-092339

Marschner, Bernard Walter (1948) An Investigation of Detached Shock Waves. Engineer's thesis, California Institute of Technology. https://resolver.caltech.edu/CaltechTHESIS:09152014-090058146

P

Parker, James Frederick and Anderson, John Berwick and Tunnell, Richard McClellan and Vincent, Harry Lansing (1946) An Investigation of the Effects of the Sudden Extension of a Dive-Recovery Flap on the Aerodynamic Characteristics of a Symmetrical Airfoil in Two Dimensional Flow. Engineer's thesis, California Institute of Technology. doi:10.7907/DJD3-KV06. https://resolver.caltech.edu/CaltechETD:etd-12022008-102010

W

Wunch, William Stuart (1948) Studies of the Double-Wedge and Biconvex Airfoils in Hypersonic Flow. Engineer's thesis, California Institute of Technology. doi:10.7907/BSMQ-5177. https://resolver.caltech.edu/CaltechETD:etd-12162008-141322

Weldon, Thomas Franklin (1947) The Performance of a Supersonic Airplane. Engineer's thesis, California Institute of Technology. doi:10.7907/T271-MK09. https://resolver.caltech.edu/CaltechETD:etd-09142005-112442

Weitzenfeld, Daniel Kehr and Trauger, Robert James and Kronmiller, George Hannibal (1946) The Effect of Dive Recovery Flaps on the Lift of a Two Dimensional Symmetrical Airfoil with Changes in Chordwise Location of the Flaps. Engineer's thesis, California Institute of Technology. doi:10.7907/CV3E-KC83. https://resolver.caltech.edu/CaltechETD:etd-11262008-112929

This list was generated on Sat May 25 11:30:22 2024 UTC.