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Jump to: 1956 | 1955 | 1954 | 1953 | 1952 | 1950 | 1949 | 1948 | 1947
Number of items: 38.

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, Lawrence Cloyd (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, Jack Carl (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 Douglas (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 Hani (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 Muin (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 Richard (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, Yusuf Amon (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

1953

DeLauer, Richard Daniel (1953) Experimental Heat Transfer at Hypersonic Mach Number. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/59SJ-TR03. https://resolver.caltech.edu/CaltechETD:etd-04222003-111626

Eimer, Manfred (1953) Direct Measurement of Laminar Skin Friction at Hypersonic Speeds. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/MK2E-1P76. https://resolver.caltech.edu/CaltechETD:etd-04292003-112020

Mackay, Douglas Severance (1953) Boundary Layer Temperature Recovery Factor on a Cone at Nominal Mach Number Six. Engineer's thesis, California Institute of Technology. doi:10.7907/8DEC-WE68. https://resolver.caltech.edu/CaltechETD:etd-05122003-095635

Stoolman, Leo (1953) Investigation of an Instability Phenomena Occurring in Supersonic Diffusors. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/EG52-8V58. https://resolver.caltech.edu/CaltechETD:etd-05122003-115303

1952

Arthur, Paul David (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

Barish, David Theodore (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 Cleveland (1950) Experimental Investigation of Detached Shock on a 70° 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 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

DeLauer, Richard Daniel (1950) Aerodynamic Characteristics of a Wedge and Cone at Hypersonic Mach Numbers. Engineer's thesis, California Institute of Technology. doi:10.7907/rndh-4a17. https://resolver.caltech.edu/CaltechThesis:09292023-233404349

Frick, Leo Francis (1950) Experimental Investigation of Detached Shock on a 70° 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, Lee Richard (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

Bacon, John William (1949) 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

Blenkush, Philip George (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 Donahue (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

Densmore, James Edward (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 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

Marx, Michael Ferdinand (1949) Low Speed Wind Tunnel Investigation of High Lift Devices on a 65° 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 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

Shonerd, David Edwin (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 William (1949) Low Speed Wind Tunnel Investigation of High Lift Devices on a 65° 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

Chuan, Raymond Lu-Po (1948) 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

Jensen, Arnold Axtell and Koerner, Warren Gottlieb (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 Jeffrey (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

Pollock, Albert David and Reck, Floyd Francis (1947) A Study of Methods to Increase the Lift of Supersonic Airfoils at Low Speeds. Engineer's thesis, California Institute of Technology. doi:10.7907/J3NG-DD26. https://resolver.caltech.edu/CaltechETD:etd-12082008-083805

This list was generated on Sun Jun 16 11:30:46 2024 UTC.