Charles F. Merlet <br/>
       Supersonic free-flight measurement of heat transfer and transition on 10 cone having a low temperature ratio.[TN D-951-TN D-960] 
 / 
 .- Washington : Nasa,  1961 
.- ( National aeronautics and space administration   
<br/>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]<br/><br/>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]<br/><br/>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]<br/><br/>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]<br/><br/>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]<br/><br/>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]<br/><br/>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]<br/><br/>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]<br/><br/>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] 
<br/><U>Author Added Entry: </u><br/>Charles B. Rumsey;
<br><U>Copy Details:</u><br> Acc. No.: <b>TR65497</b>, Full Call No.: NASA TN D-951,   Item type:  Technical Report , Location: COMPACT STORAGE (BASEMENT), <br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>