NASA Technical Note [D-2701-2710]
Contributor(s): Rolls, L. Stewart Drinkwater III, Fred J. Innis, Robert C. Reeder, John P. Clark, Louis E. Wilson, R. Gale Nixon, Charles W. Hubbard, Harvey H. Allen, Jerry M. Czarnecki, K. R. Moul, Martin T. Schy, Albert A. Whitehead, Allen H. Dunavant, James C. Corlett, William A. and Richardson, Celia S. Dolkas, Constantine B. Stewart, John D.
Material type:
BookSeries: National Aeronautics and Space Administration (NASA) NASA Technical Note.Publisher: Washington National Aeronautics and Space Administration (NASA) 1965Subject(s): Hypersonic Ceramic-Heated | Pilots Evaluation--NASA Pilots Evaluation--NASA
| 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 D2701-2710 | Not for loan | 64273 |
NASA TN D-2701: Effects of Lateral control, characteristics on hovering: jet lift vtol aircraft/ by L. Stewart Rolls, Fred J. Drinkwater III and Robert C. Innis
NASA TN D-2702: Impact of V / STOL aircraft on instrument weather operations/ John P. Reeder
NASA TN D-2703: Description and initial calibration of the langley 12-inch Hypersonic ceramic-heated tunnel/ Louis E. Clark
NASA TN D-2704: Hemispherical spectral emittance of ablation chars, carbon, and zirconia to 3700 degree K / by R. Gale Wilson
NASA TN D-2705: results of USAF-NASA-FAA flight program to study community responses to sonic booms in the greater St. Louis Area/ by Charles W. Nixon, Harvey H. Hubbard
NASA TN D-2706: Effect of surface emittance on turbulent skin friction at supersonic and low hypersonic speeds/ Jerry M. Allen and K. R. Czarnecki
NASA TN D-2707: Fixed- base simulator study of piloted entry into the earth's atmosphere at parabolic velocity/ by Martin T. Moul and Albert A. Schy
NASA TN D-2708: Study of pressure and heat transfer over an 80 degree sweep slab delta wing in hypersonic flow/ Allen H. Whitehead and James C. Dunavant
NASA TN D-2709: Effect of first-stage geometry on aerdynamic characteristics in pitch of two-stage rocket vehicles from mach 1.57 to 2.86/ by William A. Corlett and Celia S. Richardson
NASA TN D-2710: Effect of combined linear and oscillatory acceleration on pilot attitude-control capabilities/by Constantine B. Dolkas and John D. Stewart
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