Browse by Advisor

1956

Kendall, James Madison (1956) An Experimental Investigation of Leading Edge Shock Wave-Boundary Layer Interaction at Hypersonic Speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/6XVK-B331. https://resolver.caltech.edu/CaltechETD:etd-03252004-153340

1955

Baldwin, L. C. (1955) Viscous effects on static pressure distribution for a slender cone at a nominal mach number of 5.8. Engineer's thesis, California Institute of Technology. doi:10.7907/XNB2-P865. https://resolver.caltech.edu/CaltechETD:etd-11242003-104401

Howard, Weston Morgan (1955) An experimental investigation of pressure gradients due to temperature gradients in small diameter tubes. Engineer's thesis, California Institute of Technology. doi:10.7907/SQF1-5002. https://resolver.caltech.edu/CaltechETD:etd-12162003-155556

1954

Graves, J. C. (1954) Impact pressure and total temperature interpretation at hypersonic mach number. Engineer's thesis, California Institute of Technology. doi:10.7907/V04Q-TF29. https://resolver.caltech.edu/CaltechETD:etd-12182003-100211

Harkins, William D. (1954) Base pressure and static pressure for a cone-cylinder at a nominal mach number of 5.8. Engineer's thesis, California Institute of Technology. doi:10.7907/P0K8-XG38. https://resolver.caltech.edu/CaltechETD:etd-12152003-095830

Korkegi, Robert H (1954) Transition studies and skin friction measurements on an insulated flat plate at a hypersonic mach number. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/X3B9-VW73. https://resolver.caltech.edu/CaltechETD:etd-01072004-114554

Mark, Richard M. (1954) Laminar boundary layers on slender bodies of revolution in axial flow. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/4H6Z-K569. https://resolver.caltech.edu/CaltechETD:etd-01142004-155216

Quiel, Norwald R (1954) Impact pressure and total temperature interpretation at hypersonic mach numbers. Engineer's thesis, California Institute of Technology. doi:10.7907/SMHA-4160. https://resolver.caltech.edu/CaltechETD:etd-12052003-095631

Yoler, Y. A. (1954) The hypersonic shock tube. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/853G-K555. https://resolver.caltech.edu/CaltechETD:etd-02112004-115540

1952

Arthur, Paul D. (1952) Effects of impurities on the supersaturation of nitrogen in a hypersonic wind tunnel. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/PBSD-2V70. https://resolver.caltech.edu/CaltechETD:etd-03232009-152948

Buhler, Rolf Dietrich (1952) Condensation of air components in hypersonic wind tunnels : theoretical calculations and comparison with experiment. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/0J8Q-9Z82. https://resolver.caltech.edu/CaltechETD:etd-01162007-152444

Grey, Jerry (1952) The effects of air condensation on properties of flow and their measurement in hypersonic wind tunnels. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/HFHE-HR77. https://resolver.caltech.edu/CaltechETD:etd-03302009-061157

1950

Alperin, Morton (1950) A Study of Detached Shock Waves in Two-Dimensions. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/NW30-HY03. https://resolver.caltech.edu/CaltechETD:etd-02022009-081306

Bacon, J. W. (1950) An investigation of blowing as a method of increasing the maximum lift of a double-wedge airfoil. Engineer's thesis, California Institute of Technology. doi:10.7907/NT63-HE54. https://resolver.caltech.edu/CaltechETD:etd-01272009-155604

Barish, David T. (1950) Acoustical airspeed indicators. Engineer's thesis, California Institute of Technology. doi:10.7907/FR7P-K372. https://resolver.caltech.edu/CaltechETD:etd-02022009-083911

Bryan, William C. (1950) Experimental investigation of detached shock on a 70 degree cone at various angles of attack. Engineer's thesis, California Institute of Technology. doi:10.7907/XAZW-8051. https://resolver.caltech.edu/CaltechETD:etd-02042009-100038

Chase, Patrick S. (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

Frick, Leo F. (1950) Experimental investigation of detached shock waves on a 70 degree cone at various angles of attack. Engineer's thesis, California Institute of Technology. doi:10.7907/D4TV-0W57. https://resolver.caltech.edu/CaltechETD:etd-02122009-125456

Scherer, L. R. (1950) Aerodynamic characteristics of a wedge and cone at hypersonic Mach numbers. Engineer's thesis, California Institute of Technology. doi:10.7907/29PE-XX71. https://resolver.caltech.edu/CaltechETD:etd-02112009-150520

1949

Blenkush, P. G. (1949) A wind tunnel investigation of the aerodynamic characteristics of high-lift devices on supersonic wings at low subsonic speed. Engineer's thesis, California Institute of Technology. doi:10.7907/N6XA-GR06. https://resolver.caltech.edu/CaltechETD:etd-01272009-151720

Burke, James D. (1949) Sounding rocket performances analysis. Engineer's thesis, California Institute of Technology. doi:10.7907/XW5Q-1Y06. https://resolver.caltech.edu/CaltechETD:etd-01232009-152718

Chuan, Raymond Lu-Po (1949) An Investigation of Vortex Shedding as Related to the Self-Excited Torsional Oscillation of an Airfoil. Engineer's thesis, California Institute of Technology. doi:10.7907/6JQH-FS81. https://resolver.caltech.edu/CaltechETD:etd-02102009-131702

Densmore, J. E. (1949) Wind tunnel investigation of the aerodynamic characteristics of high lift devices on supersonic wings at low subsonic speed. Engineer's thesis, California Institute of Technology. doi:10.7907/Z0Y9-J658. https://resolver.caltech.edu/CaltechETD:etd-01232009-104437

MacKinnon, Neil A. (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

Marx, Michael F. (1949) Low speed wind tunnel investigation of high lift devices on a 65 degree swept-back supersonic wing of 3.44 aspect ratio. Engineer's thesis, California Institute of Technology. doi:10.7907/2B48-J790. https://resolver.caltech.edu/CaltechETD:etd-02122009-093718

Muirhead, Vincent U. (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

Shonerd, David E. (1949) Winged rocket performance analysis. Engineer's thesis, California Institute of Technology. doi:10.7907/34ZH-KG02. https://resolver.caltech.edu/CaltechETD:etd-02052009-092504

Thomas, John W. (1949) Low speed wind tunnel investigation of high lift devices on a 65 degrees swept-back supersonic wing of 3.44 aspect ratio. Engineer's thesis, California Institute of Technology. doi:10.7907/TYRW-TZ93. https://resolver.caltech.edu/CaltechETD:etd-02242009-092302

1948

Altseimer, John H. (1948) An experimental investigation of detached shock waves. Engineer's thesis, California Institute of Technology. doi:10.7907/W6SF-EG14. https://resolver.caltech.edu/CaltechETD:etd-12232008-153257

Jensen, Arnold A. (1948) Wind tunnel investigation of a supersonic tailless airplane at low subsonic speed. Engineer's thesis, California Institute of Technology. doi:10.7907/KFRK-AF65. https://resolver.caltech.edu/CaltechETD:etd-12192008-103750

Magnus, Richard J. (1948) Study of vortex shedding as related to torsional oscillations of a thin airfoil. Engineer's thesis, California Institute of Technology. doi:10.7907/NAKT-DG24. https://resolver.caltech.edu/CaltechETD:etd-12162008-142937

Marschner, Bernard Walter (1948) An investigation of detached shock waves. Engineer's thesis, California Institute of Technology. https://resolver.caltech.edu/CaltechTHESIS:09152014-090058146

1947

Dore, Frank John (1947) The design of tailless airplanes. Engineer's thesis, California Institute of Technology. doi:10.7907/0RZ6-EV10. https://resolver.caltech.edu/CaltechETD:etd-12092008-152833