Supersonic free-flight measurement of heat transfer and transition on 10 cone having a low temperature ratio.[TN D-951-TN D-960] (Record no. 566555)
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| 100 ## - MAIN ENTRY--AUTHOR NAME | |
|---|---|
| Personal name | Charles F. Merlet |
| 245 ## - TITLE STATEMENT | |
| Title | Supersonic free-flight measurement of heat transfer and transition on 10 cone having a low temperature ratio.[TN D-951-TN D-960] |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) | |
| Place of publication | Washington |
| Name of publisher | Nasa |
| Year of publication | 1961 |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE | |
| Title | National aeronautics and space administration |
| 500 ## - GENERAL NOTE | |
| General note | 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] |
| 700 ## - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Charles B. Rumsey |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | Technical Report |
| Withdrawn status | Lost status | Damaged status | Not for loan | Collection code | Permanent Location | Current Location | Date acquired | Full call number | Accession Number | Koha item type |
|---|---|---|---|---|---|---|---|---|---|---|
| COMPACT STORAGE (BASEMENT) | PK Kelkar Library, IIT Kanpur | PK Kelkar Library, IIT Kanpur | 2023-04-26 | NASA TN D-951 | TR65497 | Technical Report |