Lihat Juga

• A METHOD FOR PREDICTING FULL SCALE BUFFET RESPONSE WITH RIGID WIND TUNNEL MODEL FLUCTUATING PRESSURE DATA VOLUME I: PREDICTION METHOD DEVELOPMENT AND ASSESMENT
  oleh: NASA, WASHINGTON DC, NOVEMBER 1978
• INVESTIGATION OF STEADY AND FLUCTUATING PRESSURES ASSOCIATED WITH THE TRANSONIC BUFFETING AND WING ROCK OF A ONE-SEVENTH SCALE MODEL OF THE F-5A AIRCRAFT
  oleh: NASA, WASHINGTON DC, NOVEMBER 1978
• A WIND TUNNEL INVESTIGATION OF PANEL RESPONSE T BOUNDARY LAYER PRESSURE FLUCTUATIONS AT MACH 1.4 AND MACH 3.5
  oleh: NASA, WASHINGTON DC, MAY 1966
• CORRRELATION OF FULL SCALE DRAG PREDICTIONS WITH FLIGHT MEASUREMENTS ON THE C141A AIRCRAFT PHASE II, WIND TUNNEL TEST, ANALYSIS, AND PREDICTION TECHNIQUES VOL II
  oleh: NASA, WASHINGTON DC, FEBRUARY 1974
• CORRRELATION OF FULL SCALE DRAG PREDICTIONS WITH FLIGHT MEASUREMENTS ON THE C141A AIRCRAFT PHASE II, WIND TUNNEL TEST, ANALYSIS, AND PREDICTION TECHNIQUES VOL I
  oleh: NASA, WASHINGTON DC, FEBRUARY 1974