TRANSIENT LOADING OF WIDE DELTA-AIRFOILS AT SUPERSONIC SPEEDS

[1] LOADS ON A SUPERSONIC WING STRIKING A SHARP-EDGED GUST [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (05): : 296 - &

[2] THE TRANSIENT REACTION OF AN AIRFOIL DUE TO CHANGE IN ANGLE OF ATTACK AT SUPERSONIC SPEED [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (11): : 635 - 655

[3] HEASLET MA, 1948, NACA TN1261

[4] TRANSIENT LOADING OF AIRFOILS AT SUPERSONIC SPEEDS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (10): : 592 - 598

[5] MILES JW, 1949, RRB36 CAL TECHN MEM

[6] Peirce B.O., 1929, SHORT TABLE INTEGRAL

[7] SCHWARZ L, 1943, JB DTSCH LUFTFAHRTFO, P1

[1] LOADS ON A SUPERSONIC WING STRIKING A SHARP-EDGED GUST [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1949, 16 (05): : 296 - &

[2] THE TRANSIENT REACTION OF AN AIRFOIL DUE TO CHANGE IN ANGLE OF ATTACK AT SUPERSONIC SPEED [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (11): : 635 - 655

[3] HEASLET MA, 1948, NACA TN1261

[4] TRANSIENT LOADING OF AIRFOILS AT SUPERSONIC SPEEDS [J]. JOURNAL OF THE AERONAUTICAL SCIENCES, 1948, 15 (10): : 592 - 598

[5] MILES JW, 1949, RRB36 CAL TECHN MEM

[6] Peirce B.O., 1929, SHORT TABLE INTEGRAL

[7] SCHWARZ L, 1943, JB DTSCH LUFTFAHRTFO, P1