Skip to main content
TudRepo
Research repository
Education Repository
Cultural Heritage
About
·
How to search
·
How to upload
Include full text
Search results
Back
Searched for: +
(1 - 20 of 355)
Document type
Date
Pages
1
2
3
4
5
....
18
List view
Grid view
Print
Email
export CSV
export Excel
Report of the Advisory Committee for the William Froude National Tank for Year ending December 13st, 1925
Analog equipment for processing randomly fluctuating data
Calculation of the flow past slender delta wings with leading edge separation
Lubricant behaviour in concentrated contact. The effect of temperature
Flutter of a two-dimensional, simply supported buckled panel with elastic restraint against edge displacement
Studies of ground effect on a 60º inwardly inclined annular jet. Part II Base plate thrust augmentation and pressure distribution; effects of aspects ration, pressure ratio and height above ground; jet stability
Boundary layer growth in the nozzles of the R.A.E. 8 ft. x 8 ft. supersonic wind tunnel
An experimental method of determining the mean heat transfer coefficient for the nozzle of a solid propellant rocket engine, by means of constant flow calorimetry
The use of surface pilot tubes as skin friction meters at supersonic speeds
Study of heat and mass transfer from non-isothermal surfaces
Laboratory wave generation - A comparison of theoretical and experimental performance
An experimental assessment of the stability of the course line of an I.L.S. localiser ground equipment
An estimate of the effect of underwing nacelles on the aerodynamic efficiency of a supersonic transport aircraft
Force pulse testing of ship models
Methods and charts for estimating skin friction drag in wind tunnel tests with zero heat transfer
Some reactions of perfluoroglutaric acid
Some aspects of the thermal degradation of epoxide resins
An application of Mueller's Monte Carlo method for evaluating the stream function in a two-dimensional, irrotational, incompressible flow in a Bellmouth inlet
Measurements of skin friction on a cambered delta wing at supersonic speeds
The increase in wave drag at supersonic speeds due to surface waviness
Searched for: +
(1 - 20 of 355)
Document type
Date
Pages
1
2
3
4
5
....
18
List view
Grid view
Print
Email
export CSV
export Excel