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 / 
 .- Washigton,D.C.: National Aeronautis and Space Administration,  1964 
 .- 32p. 
.- ( National Aeronautis and Space Administration NASA Technical Note   
<br/>NASA TN-2381: Effect of wing stalling in transition on a 1/4-scale model of the vz-2 aircraft by Robert O. Schade NASA TN-2382: Force test investigation of a 1/4-scale model of the modified vz-2 aircraft by Robert H. Kirby 71p NASA TN-2383: Heat-transfer rates and ablation on a blunted cylinder-flare configuration in free flight up to a mach number of 8.98 by Clyde W. Winters 27p NASA TN-2384: Diffuser performance of a mach 6 open-jet tunnel and model-blockage effects at stagnation temperatures to 3,600 F by Raymond E. Midden 23p NASA TN-2385: Comparison of heat-rejection and weight characteristics of several radiator fin-tube configurations by Henry C. Haller 34p NASA TN-2386: Heat transfer on unswept and 38 cylindrically blunted wedge fins in free flight to mach number 4.11 by Floyd G. Howard 48p NASA TN-2387: Heat-transfer and pressure measurements on delta wings at mach numbers of 3.1 and 4.65 and angles of attack from -45 to 45 by Robert L. Stallings 176p NASA TN-2388: Vectorial reflectance of the explorer IX satellite material by Gerald M. Keating 45p NASA TN-2389: Supersonic aerodynamic characteristics of a series of bodies having variations in fineness ratio and cross-section ellipticity by Bernard Spencer,Jr.  76p NASA TN-2390: Numerical calculation of supersonic flows of a perfect gas over bodies of revolution at small angles of yaw by John V. Rakich 56p 
<br><U>Copy Details:</u><br> Acc. No.: <b>83680</b>, Full Call No.: ,   Item type:  Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D 2381-90<br><b>------------------------- --------------------- ------ --------- ------- ------- --------- -------- </b><br>