Measurments of aerodynamic heat transfer and boundary- layer transition on A 10 deg con in free flight at supersonic mach numbers up to 5.9

By Rumsey, Charles B.. Washington D. C. National Aeronautics and Space Administration (NASA) 1961 . 33p. , Bound With NASA TN D-741-750

Place Hold on Measurments of aerodynamic heat transfer and boundary- layer transition on A 10 deg con in free flight at supersonic mach numbers up to 5.9

Measurements of aerodynamic heat transfer and boundary-layer transition on a 15 deg. cone in free flight at supersonic mach numbers up to 5.2 [NASA TN D-888]

By Rumsey, Charles B.. Nasa Washington 1961 . 43p

Place Hold on Measurements of aerodynamic heat transfer and boundary-layer transition on a 15 deg. cone in free flight at supersonic mach numbers up to 5.2 [NASA TN D-888]

Supersonic free-flight measurement of heat transfer and transition on 10 cone having a low temperature ratio.[TN D-951-TN D-960]

By Charles F. Merlet. Washington Nasa 1961 , 1. Analysis of effects of interceptor roll performance and maneuver ability on success of collsion-course attacks by William H. Phillips Report NASA TN D-952 [1961] 2. Analysis of a linear system for variable-thrust control in the terminal phase of rendezvous by Richard A. hord Report NASA TN D-953 [1961] 3. A method for longitudinal and lateral range control for a high-drag low- lift vehicle entering the atmosphere of a rotating earth by John W. Young Report NASA TN D-954 [1961] 4. Heat transfer and boundary- layer transition on a highly polished hemisphere-cone in free flight at mach numbers up to 24x10 by James J. Buglia Report NASA TN D-955 [1961] 5.Incipient -and developed -spin and Recovery characteristics of a modern high-speed fighter desigh with low aspect ratio as determind from dynamic-model tests by Henry A Lee Report NASA TN D-956 [1961] 6.A study of the effect of errors in measurement of velocity and flight-path angle on the guidance of a space vehicle approaching the earth by Jack A. White Report NASA TN D-957 [1961] 7.Effects of canard planform and wing -leading-edge modification on low-speed longitudinal aerodynamic characteristics of a canard airplane configuration by Bernard spencer Jr Report NASA TN D-958 [1961] 8. Measurement of flow angularity at supersonic and hypersonic speeds with the use of a conical probe by Frank E. Swalley Report NASA TN D- 959 [1961] 9.Efffects of changing stress amplitude on the rate of fatigue-crack propagation in two aluminum alloys by C. Michael Hudson Report NASA TN D-960 [1961]

Place Hold on Supersonic free-flight measurement of heat transfer and transition on 10 cone having a low temperature ratio.[TN D-951-TN D-960]

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Measurments of aerodynamic heat transfer and boundary- layer transition on A 10 deg con in free flight at supersonic mach numbers up to 5.9

Measurements of aerodynamic heat transfer and boundary-layer transition on a 15 deg. cone in free flight at supersonic mach numbers up to 5.2 [NASA TN D-888]

Supersonic free-flight measurement of heat transfer and transition on 10 cone having a low temperature ratio.[TN D-951-TN D-960]