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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

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