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.
Contributor(s): Charles B. Rumsey.
Series: National aeronautics and space administration. Publisher: Washington Nasa 1961| Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA TN D-951 (Browse shelf) | Not for loan | TR65497 |
Browsing PK Kelkar Library, IIT Kanpur Shelves , Collection code: COMPACT STORAGE (BASEMENT) Close shelf browser
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]
There are no comments for this item.