Estimation of surface pressures from observed shock-wave envelopes surrounding conical bodies at M = 4.0 /

Measurements of pressure distribution and shock-wave shape on power-law bodies at a mach number of 6.85 /
by: Peckham, D. H.
Published: (1967)

Direct visualization of shock waves in supersonic space shuttle flight /
by: O'Farrell, J. M.
Published: (2011)

Some studies of pressure distributions on the windward surfaces of conical bodies at high supersonic speeds /
by: Akers, Arthur
Published: (1966)

Normal shock-wave tables for air, argon, carbon dioxide, carbon monoxide, hydrogen, nitrogen, nitrous oxide and oxygen /
by: Lapworth, K. C.
Published: (1970)

Gasdynamic discontinuities.
by: Hayes, Wallace D. (Wallace Dean)
Published: (1960)

Shock waves, explosions, and detonations /
Published: (1983)

Dynamics of shock waves, explosions, and detonations /
Published: (1984)

The longitudinal characteristics of three slender 'mild ogee' wings at mach numbers from 0.4 to 2.0 /
by: Mabey, Dennis G.
Published: (1968)

On the interaction of the transmitted shock with the boundary layer in a shock tube using argon as a test gas /
by: Davies, L. (Lynn), et al.
Published: (1967)

The interaction of the reflected shock with the boundary layer in a shock tube and its influence on the duration of hot flow in the reflected-shock tunnel /
by: Davies, Lynn
Published: (1967)

A study of fundamental shock noise mechanisms /
by: Meadows, Kristine R.
Published: (1997)

A note on the design and construction of a low-pressure calibrator and a comparison with shock-tube and static calibration methods /
by: Pallant, R. J.
Published: (1967)

A brief account of some unrecorded techniques for flow visualization in flight for locating (a) boundary-layer transition at altitude, (b) shock-wave position /
by: Gray, Wellington Edrington
Published: (1970)

Diffraction of blast waves for the oblique case /
by: Srivastava, Radhey Shyam, 1931-
Published: (1968)

Modification of a normal shock by electrostatic forces /
by: Butler, Geoffrey Frederick
Published: (1969)

Some comments on the conditions in a local supersonic flow region /
by: Moulden, Trevor H.
Published: (1968)

Analysis of hinge moment data for rectangular and near rectangular trailing edge controls at supersonic and transonic speeds /
by: Isaacs, Donald
Published: (1966)

Hypersonic similarity solutions for airfoils supporting exponential shock waves /
by: Cole, Julian D.
Published: (1968)

An experimental investigation of the influence of base bleed on the base drag of various propelling nozzle configurations /
by: Roberts, J. B. (Writer on aerodynamics)
Published: (1967)

Supersonic flutter derivatives for a series of swept and cropped delta wings /
by: Harris, G. Z.
Published: (1967)

Supersonic flow and shock waves /
by: Courant, Richard, 1888-1972
Published: (1948)

Mercury programmes for lifting surface theory calculations on wings oscillating in supersonic flow /
by: Harris, G. Z.
Published: (1966)

Supersonic laminar boundary layers on cones /
by: Cooke, J. C. (John Caister)
Published: (1969)

Results and analysis of pressure measurements on two isolated slender wings and slender wing-body combinations at supersonic speeds /
by: Fellows, K. A.
Published: (1970)

Characteristics of aft-mounted all-moving rectangular control surfaces on a slender cruciform model at mach numbers from 0.6 to 2.8 /
by: Winter, Kenneth George
Published: (1968)

Wind-tunnel tests on a rectangular, twin-duct, variable-geometry air intake : at supersonic speeds /
by: Dobson, M. D.
Published: (1967)

Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [as printed, as printed]. /
by: Neale, M. C.
Published: (1967)

Experimental verification of predicted static hole size effects on a model with large streamwise pressure gradients /
by: Pugh, P. G.
Published: (1971)

Optical methods for examining the flow in high-speed wind tunnels.
Published: (1957)

The performance of a conical convergent-divergent nozzle with area ratio 2.9 in external flow /
by: Golesworthy, G. T.
Published: (1967)

The performance of conical convergent-divergent nozzles of area ratios 2.44 and 2.14 in external flow /
by: Golesworthy, G. T.
Published: (1967)

Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry /
by: Herring, Gregory C.
Published: (2011)

Shock waves : proceedings of the 24th International Symposium on Shock Waves, Beijing, China, July 11-16, 2004 /
Published: (2005)

The use of air injection to prevent separation of the turbulent boundary layer in supersonic flow /
by: Peake, D. J.
Published: (1967)

Interaction of Shock Waves /
by: Srivastava, R. S.
Published: (1994)

Shock waves.