The flow field was surveyed at one station (X/D = 6.5) on an ogive- cylinder having a tangent ogive nose with a fineness ratio of 4. The surveys were performed with pitot tubes and cone pressure probes at angles of attack of 0, 5, 10 and 15 degrees for Mach numbers 3.52 and 4.07. Surface static pressures were also measured. The results of the tests are presented in tabular and plotted form. Comparisons are made with inviscid flow fields calculations and with experimental results from other investigations."24 August 1972."Includes bibliographical references (pages 40-41)The flow field was surveyed at one station (X/D = 6.5) on an ogive- cylinder having a tangent ogive nose with a fineness ratio of 4. The surveys were performed with pitot tub...
Prepared at Ames Research Center."June 1961."Cover title.Includes bibliographical references (p. 28-...
Comparisons of the development of flow over a cylinder with a 20° cone nose and a cylinder with an o...
A theoretical and experimental investigation has been conducted of the pressure distribution on the ...
The surface flow angle was measured on an ogive cylinder at angles of attack and at supersonic Mach ...
A theoretical and experimental study has been conducted of a flow field about a hemisphere-cylinder ...
Results are presented for tests conducted on a 1.5 elliptic cone to determine the pressure distribut...
Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an incline...
Wind-tunnel tests have been conducted to determine the errors of 3 seven static-pressure probes moun...
The characteristics of a 40° half-angle cone for measuring flow angularity were determined experimen...
A series of dynamic flow field pressure probes were developed for use in large-scale supersonic wind...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
The static pressure distribution on sharp and blunt 10-deg half-angle cones was measured under raref...
This test was conducted in support of a program to develop a generalized analytical method for predi...
An experimental program was conducted to survey the lee side vortex flow field about an ogive-cylind...
Transient pressures, induced by wind-tunnel simulated head-on blast wave interactions, have been mea...
Prepared at Ames Research Center."June 1961."Cover title.Includes bibliographical references (p. 28-...
Comparisons of the development of flow over a cylinder with a 20° cone nose and a cylinder with an o...
A theoretical and experimental investigation has been conducted of the pressure distribution on the ...
The surface flow angle was measured on an ogive cylinder at angles of attack and at supersonic Mach ...
A theoretical and experimental study has been conducted of a flow field about a hemisphere-cylinder ...
Results are presented for tests conducted on a 1.5 elliptic cone to determine the pressure distribut...
Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an incline...
Wind-tunnel tests have been conducted to determine the errors of 3 seven static-pressure probes moun...
The characteristics of a 40° half-angle cone for measuring flow angularity were determined experimen...
A series of dynamic flow field pressure probes were developed for use in large-scale supersonic wind...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
The static pressure distribution on sharp and blunt 10-deg half-angle cones was measured under raref...
This test was conducted in support of a program to develop a generalized analytical method for predi...
An experimental program was conducted to survey the lee side vortex flow field about an ogive-cylind...
Transient pressures, induced by wind-tunnel simulated head-on blast wave interactions, have been mea...
Prepared at Ames Research Center."June 1961."Cover title.Includes bibliographical references (p. 28-...
Comparisons of the development of flow over a cylinder with a 20° cone nose and a cylinder with an o...
A theoretical and experimental investigation has been conducted of the pressure distribution on the ...