A short time response stagnation temperature probe /

Nitrogen condensation in the R.A.R.D.E. hypersonic gun tunnel /
by: Bowman, J. E.
Published: (1967)

Bulk compressibility effects in the R.A.R.D.E. no. 3 hypersonic gun tunnel /
by: Clayden, W. A.
Published: (1966)

Thermophysical aspects of re-entry flows /
Published: (1986)

Aerospace thermal structures and materials for a new era /
Published: (1995)

Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) /
by: Marroquin, J.
Published: (1985)

A long stroke isentropic free piston hypersonic wind tunnel /
by: East, R. A.
Published: (1980)

Experimental investigation of hexcomb-pattern roughness effects on transition onset and turbulent heating augmentation at Mach 6 /
by: Hollis, Brian R. (Brian Ray)
Published: (2019)

Advanced hypersonic test facilities /
Published: (2002)

Supersonic interference flow along the corner of intersecting wedges /
by: Charwat, A. F.
Published: (1966)

A generalized analysis of the performance characteristics and operating ranges of hypersonic-flow test facilities. /
by: Charwat, A. F.
Published: (1965)

The Imperial College graphite heated hypersonic windtunnel /
by: Harvey, John (John K.)
Published: (1972)

Nonequilibrium hypersonic aerothermodynamics /
by: Park, Chul, 1934-
Published: (1990)

Some comments on air condensation effects in a hypersonic helium tunnel /
by: Davies, L.
Published: (1971)

Air condensation effects measured in the R.A.E. 7 in. x 7 in. hypersonic wind tunnel /
by: Crane, John Frank William
Published: (1968)

Advances in hypervelocity techniques ; proceedings /

Experimental methods of hypersonics /
by: Lukasiewicz, J.
Published: (1973)

The response times of typical transducer-tube configurations for the measurement of pressures in high-speed wind tunnels /
by: Larcombe, M. J.
Published: (1966)

The hypersonic viscous shock layer with mass transfer /
by: Chen, S. Y.
Published: (1966)

Arc heaters and MHD accelerators for aerodynamic purposes ; Proceedings of a specialists meeting, sponsored /
Published: (1964)

Three articles for McGraw-Hill encyclopedia of science & technology /
by: Chen, S. Y.
Published: (1968)

Subsonic tests in free molecule flow on impact tube pressure probes having a wide range of tube lengths at angles of attack up to 90 ̊ /
by: Hughes, Peter C. (Peter Carlisle), 1940-
Published: (1965)

The accuracy of pressure transducers when used in short-duration wind-tunnel facilities /
by: Pennelegion, L.
Published: (1967)

An analogue computer for on-line correction of wind-tunnel force and moment data /
by: Pecover, B. E.
Published: (1967)

Heat transfer and transition measurements at M=8.5 on a delta model and a flat plate at incidence /
Published: (1969)

Theories and technologies of hypervelocity shock tunnels /
by: Jiang, Z. (Zonglin), et al.
Published: (2023)

The high temperature aspects of hypersonic flow proceedings of the AGARD-NATO Specialists' Meeting sponsored by the Fluid Dynamics Panel of AGARD, held at the Technical Centre for Experimental Aerodynamics, Rhode-Saint-Genèse, Belgium, 3-6 April 1962.
Published: (1964)

Basics of aerothermodynamics /
by: Hirschel, Ernst-Heinrich
Published: (2005)

Tests at a mach number of 2.0 on a rectangular twin-duct air intake with variable geometry : situated in the flow field of a slender wing /
by: Dobson, M. D.
Published: (1970)

Wall corrections to longitudinal components measured on wind-tunnel models with tails /
by: Lovell, D. A.
Published: (1969)

Characteristics of high-speed wind tunnels in the United Kingdom relevant to aeroelastic-model tests /
by: Irwin, C. A. K.
Published: (1967)

A technique for the wind tunnel simulation of store release at high speeds /
by: Beecham, L. J.
Published: (1966)

The influence of density gradients on the effectiveness of film cooling /
by: Pai, B. R.
Published: (1968)

The mothball, sustainment, and proposed reactivation of the hypersonic tunnel facility (HTF) at NASA Glenn Research Center Plum Brook Station /
by: Thomas, Scott R.
Published: (2010)

A method for correcting measurements of the heat transfer factor through the skin of a wind tunnel model /
by: Piggott, Brian Alexander Martin
Published: (1966)

The new system for controlling the attitude and motivator deflections of a model in the R.A.E. No. 19 wind tunnel /
by: Pecover, B. E.
Published: (1968)

A simple flexible supersonic wind tunnell nozzle for the rapid and accurate variation of flow mach number /
by: Pierce, D.
Published: (1967)