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 / 
 .- Washington, D. C.: National Aeronautics and Space Administration,  1969 
 .- 33p. 
.- ( National Aeronautics and Space Administration NASA Technical Note   
<br/>NASA TN D-4891: Prediction of lift and drag for slender sharp-edge delta wings in ground proximity by Charles H. Fox 33p NASA TN D-4892: Rotational and vibrational temperature measurements in the 12-inch hypersonic ceramic heated tunnel by John C. Hope 35p NASA TN D-4893: Analysis of commutated networks employing feedback circuits by Michael T. Borelli 85p NASA TN D-8994: Blast shields testing by Walter V. Medenica 59p NASA TN D-4895: Optimum design of communication links with noisy phase reference by William E. Zurubek 22p NASA TN D-4896: Response develope- A global description of three axix large angle spacecraft attitutude control systems by George Meyer 31p NASA TN D-4897: Transient solidification outside a cooled pipe application to a solar brayton heat receiver by Wellington W. Hu 30p NASA TN D-4898: Design and analysis of a modular servoamplifier for fast response electrhydrraulic control systems by John R. Zeller 20p NASA TN D-4899: Prediction of thermodynamic effects of developed gavitation based on liquid hydrogen and freon-114 data in scaled ventures by Royce D. Moore 22p 
<br><U>Copy Details:</u><br> Acc. No.: <b>101120</b>, Full Call No.: ,   Item type:  Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D 4891-4899<br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>