AERADE Home
→
Browsing by Author

Browsing by Author "C. S. Brown"

Now showing items 1-8 of 8

An experimental and theoretical comparison at M=4 of the lift-to-drag ratio of some possible aircraft shapes

C. S. Brown; E. L. Goldsmith (1967)

Summary. An experimental and theoretical comparison has been made between two different methods of combining excess cross-sectional area (due to the engine exhaust nozzle exit being larger than the intake entry) with the ...
Heat transfer in the vicinity of a 15 degrees compression corner at mach numbers from 2.5 to 4.4

R. C. Hastings; C. S. Brown; Susan Atkinson (1967)
Loads on a model during starting and stopping of an intermittent supersonic wind tunnel

K. G. Winter; C. S. Brown (1957)
Measurement of the Internal Performance of a Rectangular Air Intake having Variable Geometry Compression Surfaces at Mach Numbers from 1.7 to 2.5. Part 11 The Effect of Incidence

C. S. Brown; E. L. Goldsmith (1973)

Measurements have been made of the internal performance of a rectangular intake having variable geometry compression surfaces. The measurements have been made within a range of Mach numbers from 1.7 to 2.46 and at angles ...
Measurement of the internal performance of a rectangular air intake mounted on a fuselage at mach numbers from 1.6 to 2 part 4

C. S. Brown; E. L. Goldsmith (1974)
Measurement of the internal performance of a rectangular air intake with variable geometry at mach numbers from 1.7 to 2.5 part 1

C. S. Brown; E. L. Goldsmith (1973)
Measurement of the internal performance of a rectangular air-intake at a mach number of 0.9

C. S. Brown; E. L. Goldsmith (1976)
The use of an araldite coated iron casting as a liner for a supersonic wind tunnel

C. S. Brown; K. G. Winter (1957)

Browsing by Author "C. S. Brown"

Browsing by Author "C. S. Brown"

Search AERADE

Browse

All of AERADE

My Account