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By: Washington: National Aeronautis and Space Administration.
Material type:
BookSeries: National Aeronautis and Space Administration ; NASA Technical Note. Publisher: Washigton,D.C. National Aeronautis and Space Administration 1964Description: 32p.
| Item type | Current location | Collection | Call number | Vol info | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA TN D 2381-90 | Not for loan | 83680 |
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
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