Number of items: 33.
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
This list was generated on Mon Feb 6 11:31:39 2023 UTC.