Number of items: 42.
A
Ashkenas, Irving Louis
(1939)
Wind tunnel model tests to investigate the effects of boundary layer control.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-05222007-104409
B
Burke, James D.
(1949)
Sounding rocket performances analysis.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-01232009-152718
Bell, Richard William
(1941)
Some aspects of the effects of propeller operation on the static longitudinal stability of an airplane.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-12012008-095536
Belsley, Steven E.
(1940)
The determination of two parameters dealing with power-on stability for a model with right hand propellers.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-11142008-131655
Bolster, Calvin M.
(1936)
Wind tunnel tests on the effect of power on the stability of a low wing monoplane with three vertical positions of horizontal tail surfaces.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-01102006-161025
C
Charters, Alexander C.
(1938)
The effect of curvature on boundary layer transition.
Dissertation (Ph.D.), California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-04292008-110647
D
Davidson, Harold William
(1951)
Lift increase obtained with boundary layer suction on a 10% double wedge airfoil with a 20% chord leading and trailing edge flaps.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-03192009-110707
Dilworth, J. A.
(1941)
An analytical approach to the problem of longitudinal stability of flying boats in the planing conditions.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-11202008-130754
F
Fehrman, Alvin L
(1955)
Effect of spin and yaw on boundary layer transition along a body of revolution.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-12092003-160300
Fischer, C. Fink
(1941)
The performance of jet propelled space vehicles.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechTHESIS:04192011-133614556
Fleming, M. K.
(1936)
Experimental investigation of the effect of power upon the static longitudinal stability of a low winged monoplane and a method for its calculation.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-04152008-085638
G
Gibbons, R. M. and Dill, Douglas
(1942)
A photoelastic investigation of the effect of elliptical and modified cutouts in flat panels subjected to combined bending and shear.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechTHESIS:08242010-095944937
Goode, John Edward
(1942)
Maneuverability.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-11142008-113423
H
Huebner, Danny Frederick
(1958)
Experimental development of a short flexible plate nozzle using the influence method.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-11012004-143034
Hanger, W. M.
(1943)
A photoelastic investigation of the effect of elliptical and modified cutouts in flat panels subjected to combined bending and shear.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-11182008-133221
Hatton, George A.
(1940)
The longitudinal stability of a flying-boat in the planing condition as computed from tank test data of a hull model.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-11142008-082321
K
Kiergan, Nova B.
(1942)
A study of flutter in one degree of freedom.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-11242008-082928
Knoblock, F. D.
(1939)
Investigations on the applications of the hot wire anemometer for turbulence measurements.
Dissertation (Ph.D.), California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-04252008-094935
Koch, Walter Louis
(1939)
An experimental investigation of wind tunnel wall interference on rolling and yawing moments due to deflected ailerons.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-10282005-141733
L
Larsen, H. C.
(1955)
Design of a model for the measurement of the pressure ditribution on an axially symmetric rotating body.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-03312009-095556
Losey, R. M.
(1937)
A theoretical investigation of the possibilities of internal cooling of aircraft engines by water injection to the cylinder.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-04112008-132848
M
McMahon, Howard Martin
(1958)
An experimental study of the effect of mass injection at the stagnation point of a blunt body.
Dissertation (Ph.D.), California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-01262006-142812
Miller, Herman
(1948)
Investigation of errors obtained with reflection-plane mounted models due to end plate tares.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-12192008-104129
N
Nay, Harvey O.
(1952)
Low speed boundary layer and pressure distribution tests on a family of swept back wings.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-03302009-081125
Nagashi, Mashiro
(1931)
A study of fully developed turbulent flow at a very high Reynolds number.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-06142006-110528
O
Oliver, Robert E.
(1957)
Part I. The effect of a simple throat distortion on the downstream flow in a hypersonic wind tunnel nozzle. Part II. An experimental investigation of flow over simple blunt bodies at a nominal Mach number of 5.8.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-07152004-105812
Oswald, Telford Wilbert
(1951)
The influence of variable air density and of nonlinear aerodynamic characteristics on dynamic behavior at supersonic speeds.
Dissertation (Ph.D.), California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-02242006-160420
Oswald, W. Bailey
(1932)
The transverse force distribution on ellipsoidal and nearly ellipsoidal bodies moving in an arbitrary potential flow.
Dissertation (Ph.D.), California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-09062007-141717
P
Powell, Walter B.
(1940)
An investigation of some problems in the design of tailless airplanes.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-11252008-112304
Pai, Shih-I
(1939)
On turbulent flow between rotating cylinders.
Dissertation (Ph.D.), California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-01092006-143245
Piper, Clark Neill
(1939)
Experimental investigation of the profile drag and boundary layer of a wing section during free flight and in the wind tunnel.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-01092006-142449
S
Schmidt, Louis Vincent
(1950)
Investigation of blockage effects from flow about circular cylinders in a two-dimensional wind tunnel.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechTHESIS:09302010-144157909
Seager, Donald B.
(1948)
Operational flight testing.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-12162008-153900
Smith, Josiah E.
(1948)
Investigations of the aerodynamic interactions between wind tunnel models and their support systems at the GALCIT ten foot wind tunnel.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechTHESIS:05112011-092002748
Schamberg, Richard
(1947)
The fundamental differential equations and the boundary conditions for high speed slip-flow, and their application to several specific problems.
Dissertation (Ph.D.), California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-12272004-161736
Shevell, Richard Shepherd
(1942)
The design and testing of an aerodynamic model of a high speed wind tunnel.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-11192008-145939
Scoles, Albert B.
(1938)
Range calculations for airplanes with continuously controllable pitch propellers, and the effect of certain geometric parameters of the airplane on range.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-02082006-090132
Smith, A. M. O.
(1938)
A preliminary study of the problem of boundary layer control.
Master's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-12052007-091749
T
Thorman, H. Carl
(1958)
Boundary layer measurements on an axisymmetric body with spin and yaw.
Dissertation (Ph.D.), California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-01192006-132244
Trilling, Leon
(1947)
A problem in potential flow with a free surface.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-12102008-144858
W
Wheldon, Wilbert G.
(1948)
Method for estimating downwash behind swept airfoils.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-12152008-143236
Williams, Edgar P.
(1942)
Fuselage and nacelle effects on airplanes as determined by a statistical study of data from the GALCIT 10-foot tunnel.
Engineer's thesis, California Institute of Technology.
http://resolver.caltech.edu/CaltechETD:etd-01282009-104914
This list was generated on Fri May 24 02:30:49 2013 PDT.
