College of Aeronautics
149 published titles
Stresses in a stiffened circular cylinder under concentrated axial loads
1 edition
The low speed performance of related aerofoils in cascades
1 edition
Research work in aircraft structures
1 edition
The equations of motion and energy and the velocity profile of a turbulent boundary layer in a compressible fluid
1 edition
- College of Aeronautics
- 1951
- Details
The evaluation of matrix elements for the analysis of swept-back wing structures by the method of oblique co-ordinates
1 edition
- College of Aeronautics
- 1951
- Details
Measurement of the pressure distribution on swept-back wings with trailing edge split flaps
1 edition
- College of Aeronautics
- 1951
- Details
Tests on the general instability of a stiffened metal cylinder under axial compression
1 edition
- College of Aeronautics
- 1951
- Details
The use of a potential flow tank for testing axi-symmetric contraction shapes suitable for wind tunnels
1 edition
- College of Aeronautics
- 1951
- Details
Vibrations of a swept box
1 edition
- College of Aeronautics
- 1951
- Details
A method of designing corner channels and cascades on a hyperbolic base-line
1 edition
Stability of the compressible laminar boundary layer with an external pressure gradient
1 edition
- College of Aeronautics
- 1951
- Details
Theoretical stability derivatives of a highly swept delta wing and slender body combination
1 edition
- College of Aeronautics
- 1951
- Details
Stress distribution near a rectangular cut-out in a reinforced circular cylinder due to direct shear loading and torque. Part 1, Test results
1 edition
- College of Aeronautics
- 1952
- Details
Aileron reversal and divergence of swept wings with special consideration of the relevant aerodynamic and elastic characteristics
1 edition
- College of Aeronautics
- 1952
- Details
The diffusion of transverse loads in a reinforced circular cylinder with non-rigid frames
1 edition
The distribution of pressure over the surface of wings of small aspect ratio Eby W.S.D. Marshall
1 edition
- College of Aeronautics
- 1952
- Details
An investigation of the noise field from a small jet and methods for its reduction
1 edition
- College of Aeronautics
- 1952
- Details
The determination in flight of the body drag and the mean blade profile drag coefficient of a helicopter
1 edition
- College of Aeronautics
- 1952
- Details
The theory of general instability of cylindrical shells
1 edition
- College of Aeronautics
- 1952
- Details
An investigation of the flexure-torsion flutter characteristics of aerofoils in cascade
1 edition
- College of Aeronautics
- 1952
- Details
Effects of rate and duration of loading on the strength of aircraft structures
1 edition
The potential due to a source moving through a compressible fluid and applications to some rotary derivatives of an aerofoil
1 edition
- College of Aeronautics
- 1952
- Details
List of reports 1-16
1 edition
- Cranfield College of Aeronautics
- 1952
- Details
Surface conduction of the heat transferred from a boundary layer
1 edition
- College of Aeronautics
- 1952
- Details
Optimum climb technique for a jet propelled aircraft
1 edition
- College of Aeronautics
- 1952
- Details
Service failures in aircraft structures associated with fatigue,repeated or dynamic loads
1 edition
An electric tank for the determination of theoretical velocity distributions
1 edition
The laminar boundary layer in slip flow
1 edition
- College of Aeronautics
- 1952
- Details
On some aspects of the noise propagation from supersonic aircraft
1 edition
- College of Aeronautics
- 1953
- Details
Analysis of two-cell swept box with ribs parallel to the line of flight under loading by constant couples
1 edition
- College of Aeronautics
- 1953
- Details
A note on the estimation of some low speed characteristics of delta wings
1 edition
- College of Aeronautics
- 1953
- Details
The two-dimensional laminar boundary layer at hypersonic speeds
1 edition
- College of Aeronautics
- 1953
- Details
Note on research into some aspects of stall warning devices
1 edition
- College of Aeronautics
- 1953
- Details
The calculation of the profile drag of aerofoils and bodies of revolution at supersonic speeds
1 edition
- College of Aeronautics
- 1953
- Details
Some experiments on the flow in the boundary layer of a 45° sweptback untapered wing of aspect ratio 4
1 edition
- College of Aeronautics
- 1953
- Details
The diffusion of load into a semi-infinite sheet. Parts 1 and 2
1 edition
Some tests on compressor cascades of related aerofoils having different positions of maximum camber
1 edition
The measurement of the overall drag of an aircraft at high mach numbers
1 edition
Analysis of experiments on swept wing structures
1 edition
- College of Aeronautics
- 1953
- Details
The instrumentation of an aircraft (de Havilland "Dove") for flight test instruction
1 edition
- College of Aeronautics
- 1953
- Details
Note on the development of a trailing-edge flap as a stall detector
1 edition
- College of Aeronautics
- 1953
- Details
An approximate solution of the compressible laminar boundary layer on a flat plate
1 edition
The theoretical wave drag at zero lift of fully-tapered swept wings of arbitrary section
1 edition
- College of Aeronautics
- 1953
- Details
Testing and analysis of a 60° swept back wing with ribs parallel to the line of flight
1 edition
- College of Aeronautics
- 1953
- Details
Records of major strength tests
1 edition
Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers)
1 edition
- College of Aeronautics
- 1954
- Details
Stress concentration swept wing panels using photoelastic models
1 edition
- College of Aeronautics
- 1954
- Details
A résumé of maximum lift data for symmetrical wings with various high lift aids
1 edition
- College of Aeronautics
- 1954
- Details
An experimental investigation of the pressure distribution on five bodies of revolution at Mach numbers of 2.45 and 3.19
1 edition
- College of Aeronautics
- 1954
- Details
The economics of aircraft production : a study of the control of overhead costs in aircraft manufacture
1 edition
- College of Aeronautics
- 1954
- Details
The drag increase at high subsonic speeds
1 edition
A bibliography and survey of the vortex tube
1 edition
- Cranfield College of Aeronautics
- 1954
- Details
Some bearing materials under high pressures at low rotational speeds
1 edition
- College of Aeronautics
- 1954
- Details
Investigation into the machining of titanium 150A in the forged state
1 edition
- Cranfield College of Aeronautics
- 1954
- Details
Note on the results of some profile drag calculations for a particular body of revolution at supersonic speeds
1 edition
- College of Aeronautics
- 1954
- Details
The wave drag of highly swept wings : a comparison of linear theory and slender body theory
1 edition
- College of Aeronautics
- 1954
- Details
The calculation of wave drag of a family of low-drag axi-symmetric nose shapes of fineness ratio 4.5 at zero incidence at supersonic speeds
1 edition
- Cranfield College of Aeronautics
- 1954
- Details
Solution of a load diffusion problem by relaxation methods
1 edition
- College of Aeronautics
- 1954
- Details
Vibration characteristics of a cantilever plate with swept-back leading edge
1 edition
- College of Aeronautics
- 1954
- Details
Plastic tools for aircraft production
1 edition
- College of Aeronautics
- 1955
- Details
The drag of source distributions in linearized supersonic flow
1 edition
- College of Aeronautics
- 1955
- Details
Protection of aircraft fuel tanks against explosion hazards using inert combustion products
1 edition
- College of Aeronautics
- 1955
- Details
The application of memo-motion to industrial operation
1 edition
- College of Aeronautics
- 1955
- Details
The combustion characteristics of a cylindrical-rod burner system
1 edition
- Cranfield College of Aeronautics
- 1955
- Details
The application of sub-sonic vibrations during solidification of castings with particular reference to a material for gas turbine blades- 'H.R.Crown Max'
1 edition
- Cranfield College of Aeronautics
- 1955
- Details
Investigation of eye movements of an aircraft pilot under blind approach conditions
1 edition
- College of Aeronautics
- 1955
- Details
Proceedings of the Second Work Study School Conference, Cranfield, 1955
1 edition
- College of Aeronautics
- 1955
- Details
Work study in Germany : a report of the activities of REFA
1 edition
- College of Aeronautics
- 1955
- Details
A framework for compensating rest allowance
1 edition
- College of Aeronautics
- 1955
- Details
The effect of vibrations on the mechanical properties of H.R.Crown Max and Nimonic C.75
1 edition
- Cranfield College of Aeronautics
- 1955
- Details
Low speed wind tunnel calibration of a Mk.9A pitot-static head
1 edition
On the synthesis of 3-terminal RC networks
1 edition
- Cranfield College of Aeronautics
- 1956
- Details
An approximate solution to the swept wing root constraint problem
1 edition
- College of Aeronautics
- 1956
- Details
The flexure-torsion flutter of cambered aerofoils in cascade
1 edition
- Cranfield College of Aeronautics
- 1956
- Details
A method for the numerical evaluation of an integral (occurring in the expression for the wave drag of slender bodies
1 edition
- College of Aeronautics,Cranfield
- 1956
- Details
Investigations into a photoelastic method for the direct measurement of surface strains in metal components
1 edition
- College of Aeronautics
- 1956
- Details
Double shear strength of BSL 69 snap head rivets in L.72 and L.73 aluminium alloy sheet
1 edition
- Cranfield College of Aeronautics
- 1956
- Details
The free streamline method applied to the flow at the rear of a duct
1 edition
- College of Aeronautics
- 1956
- Details
A potential flow model for the flow about a nacelle with jet
1 edition
- College of Aeronautics
- 1956
- Details
Notes on the theory of planar electric networks
1 edition
- Cranfield College of Aeronautics
- 1956
- Details
Characteristics of the flow field over the mid-upper fuselage of Lancaster P.A.474
1 edition
- College of Aeronautics
- 1956
- Details
The effect of transition wires on the pressure distribution over a N.A.C.A. 62A215 aerofoil section
1 edition
- College of Aeronautics
- 1956
- Details
Note on working speeds of some basic clerical operations
1 edition
- College of Aeronautics
- 1956
- Details
An automatic recording spectrophotometer
1 edition
- College of Aeronautics
- 1956
- Details
The influence of engine speed upon pre-ignition
1 edition
- Cranfield College of Aeronautics
- 1956
- Details
A preliminary report on the design and performance of ducted windmills
1 edition
- Cranfield College of Aeronautics
- 1956
- Details
The flow at the mouth of a Stanton pitot
1 edition
Four papers contributed by members of the staff and published on the occasion of the 10th anniversary of its foundation
1 edition
- Cranfield College of Aeronautics
- 1956
- Details
The air resistance of racing cycists
1 edition
- College of Aeronautics
- 1956
- Details
The displacement effect of pitot tubes in narrow wakes
1 edition
- College of Aeronautics
- 1956
- Details
Certain methods of stress-analysis of rectangular multi-web box beams
1 edition
- College of Aeronautics
- 1956
- Details
Production, employment and productivity in the United Kingdom,1948-55
1 edition
- Cranfield College of Aeronautics
- 1956
- Details
Method study of hot working conditions
1 edition
- College of Aeronautics
- 1956
- Details
Machinability of ultra high tensile steel
1 edition
- College of Aeronautics
- 1957
- Details
Strength of Avdel light alloy blind rivets in DTD 546 B sheet
1 edition
- Cranfield College of Aeronautics
- 1957
- Details
On the choice of working fluid for intermittent supersonic wind tunnels
1 edition
- College of Aeronautics
- 1957
- Details
Experiments on pitot-tubes in shear flow
1 edition
Independence of helicopter rotor derivatives under nonuniformity of induced velocity distribution at low forward speed
1 edition
- College of Aeronautics
- 1957
- Details
Spontaneous-ignition data of hydrocarbons and aviation fluids
1 edition
- College of Aeronautics
- 1957
- Details
A method of optimising aircraft autostabilizer systems
1 edition
- College of Aeronautics
- 1957
- Details
Vortex tube performance data sheets
1 edition
- College of Aeronautics
- 1957
- Details
Water injection in the normally-aspirated piston engine
1 edition
- Cranfield College of Aeronautics
- 1957
- Details
Initial aircraft weight prediction
1 edition
- College of Aeronautics
- 1957
- Details
The design of a multi-cell box in pure bending for minimum weight
1 edition
- College of Aeronautics
- 1957
- Details
The effect of combustor outlet temperature profiles on ramjet thrust
1 edition
- College of Aeronautics
- 1957
- Details
Notes on the problem of the optimum design of structures
1 edition
- College of Aeronautics
- 1958
- Details
A variable delay line
1 edition
- College of Aeronautics
- 1958
- Details
Discontinuity stresses at the junction of a pressurised spherical shell and a cylinder
1 edition
- College of Aeronautics
- 1958
- Details
Investigation into the use of Freon 12 as a working medium in a high-speed wind-tunnel
1 edition
- College of Aeronautics
- 1958
- Details
Theory of structural design
1 edition
- College of Aeronautics
- 1958
- Details
Pressure probes selected for three-dimensional flow measurement
1 edition
Thermal stresses in thin cylindrical shells stiffened by plane bulkheads for arbitrary temperature distributions
1 edition
- College of Aeronautics
- 1958
- Details
Thermal stresses in a box structure
1 edition
- College of Aeronautics
- 1958
- Details
Atmosphere breathing engines in astronautics
1 edition
- College of Aeronautics
- 1958
- Details
The exact flow behind a yawed conical shock
1 edition
- College of Aeronautics
- 1958
- Details
Subsonic drag and pitching moment characteristics of slender cambered bodies
1 edition
- College of Aeronautics
- 1958
- Details
The flow of chemically reacting gas mixtures
1 edition
- Cranfield College of Aeronautics
- 1958
- Details
High altitude and satellite rockets : a symposium held at Cranfield, England, 18th-20th July 1957
(Contributor)
1 edition
- Royal Aeronautical Society
- 1958
- Details
Effect of body incidence on two afterbodies with a rearward facing jet
1 edition
- College of Aeronautics
- 1958
- Details
Notes on some simple strain gauge networks commonly used with wind tunnel balances
1 edition
Some experiments with static tubes at transonic speeds in a slotted-wall wind tunnel
1 edition
Aviation fuel problems at high altitudes and high aircraft speeds
1 edition
- College of Aeronautics
- 1959
- Details
Graphite as a structural material in conditions of high thermal flux
1 edition
- College of Aeronautics
- 1959
- Details
The two-dimensional flow of an ideal dissociating gas
1 edition
- College of Aeronautics
- 1959
- Details
The dynamic loading of spur gear teeth
1 edition
- College of Aeronautics
- 1959
- Details
Property requirements for liquid rocket propellants
1 edition
- College of Aeronautics
- 1959
- Details
Ablation studies of low melting point bodies in a pre-heated supersonic air stream
1 edition
- College of Aeronautics
- 1960
- Details
On the sudden contact between a hot gas and a cold solid
1 edition
- College of Aeronautics
- 1960
- Details
On surface pressure fluctuations in turbulent boundary layer
1 edition
- College of Aeronautics
- 1960
- Details
A simplified theory of skin friction and heat transfer for a compressible laminar boundary layer
1 edition
- College of Aeronautics
- 1960
- Details
The aerodynamic derivatives of an aerofoil oscillating in an infinite staggered cascade
1 edition
- College of Aeronautics
- 1960
- Details
An elementary study of gas injection and sublimation into a simple shear layer
1 edition
- College of Aeronautics
- 1960
- Details
Dislocations and twinning in graphite
1 edition
- College of Aeronautics
- 1960
- Details
Dynamics of fuel in tanks
1 edition
- College of Aeronautics
- 1960
- Details
Base pressure at subsonic speeds in the presence of a supersonic jet
1 edition
- College of Aeronautics
- 1960
- Details
Heat conduction through a gas with one inert internal mode
1 edition
- College of Aeronautics
- 1960
- Details
An extension of Multhopp's lifting surface theory
1 edition
- College of Aeronautics
- 1960
- Details
Pressure and boundary layer measurements on a tapered swept wing in flight
1 edition
- College of Aeronautics
- 1960
- Details
Ground level disturbance from large aircraft flying at supersonic speeds
1 edition
- College of Aeronautics
- 1960
- Details
Pressure fluctuations in an incompressible turbulent boundary layer
1 edition
- College of Aeronautics
- 1960
- Details
Temperature effects on material characteristics
1 edition
- College of Aeronautics
- 1960
- Details
The role of motorists in motorcycle safety : a preliminary examination in terms of (a) motorcyclists' opinions of motorist culpability and (b) the influence of motorcycling experience on motorists' op
(Contributor)
1 edition
- ISBN: 0947767193
- Cranfield College of Aeronautics, College of Aeronautics
- 1985
- Details
Ground effect on a rotor wake
(Contributor)
1 edition
- ISBN: 0947767215
- College of Aeronautics, Cranfield Institute of Technology
- 1985
- Details
Full scale and wind tunnel surface pressure measurements on the T.R.R.L. spray dispersion programme vehicles
(Contributor)
1 edition
- ISBN: 0947767800
- College of Aeronautics
- 1987
- Details
The aerodynamic design optimisation of a forward swept wing fighter aircraft
(Contributor)
1 edition
- ISBN: 0947767835
- College of Aeronautics, Cranfield Institute of Technology
- 1987
- Details
Multidimensional WAF-type schemes for model conservation laws
(Contributor)
1 edition
- ISBN: 1871564654
- College of Aeronautics, Cranfield University
- 1993
- Details
Wind tunnel tests on a variable camber wing
(Contributor)
1 edition
- ISBN: 1871564786
- College of Aeronautics
- 1993
- Details
GENENG : a generic turboprop engine model
(Contributor)
1 edition
- ISBN: 1871564794
- College of Aeronautics
- 1996
- Details
GeoSAR : summary of the group design project, MSc in Astronautics and Space Engineering, 2005/06, Cranfield University
(Contributor)
1 edition
- ISBN: 9781861941244
- Cranfield Space Research Centre, Cranfield University
- 2006
- Details