000			02059nam a22003017a 4500
003			OSt
005			20220922095318.0
008			220922b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
110			_aWashington: National Aeronautis and Space Administration
245			_a-
260			_aWashigton,D.C. _bNational Aeronautis and Space Administration _c1964
300			_a32p
440			_aNational Aeronautis and Space Administration
440			_aNASA Technical Note
500			_aNASA TN-2381: Effect of wing stalling in transition on a 1/4-scale model of the vz-2 aircraft by Robert O. Schade
500			_aNASA TN-2382: Force test investigation of a 1/4-scale model of the modified vz-2 aircraft by Robert H. Kirby 71p
500			_aNASA 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
500			_aNASA 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
500			_aNASA TN-2385: Comparison of heat-rejection and weight characteristics of several radiator fin-tube configurations by Henry C. Haller 34p
500			_aNASA 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
500			_aNASA 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
500			_aNASA TN-2388: Vectorial reflectance of the explorer IX satellite material by Gerald M. Keating 45p
500			_aNASA TN-2389: Supersonic aerodynamic characteristics of a series of bodies having variations in fineness ratio and cross-section ellipticity by Bernard Spencer,Jr. 76p
500			_aNASA 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
942			_cTR
999			_c566156 _d566156