NASA / TN D-620 -
Charles F Whitcomb
Investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30(degree) sweptback wing at transonic speeds / .- ,
Author Added Entry:
Philippa F Brown;
Copy Details:
Acc. No.: TR10235, Full Call No.: NASA TN D-620 -, Item type: Technical Report , Location: General Stacks,
------------------------- --------------------- ------ --------- ------- ------- --------- --------
Charles F Whitcomb
Investigation of wing and aileron loads due to deflected inboard and outboard ailerons on a 4-percent-thick 30(degree) sweptback wing at transonic speeds / .- ,
Author Added Entry:
Philippa F Brown;
Copy Details:
Acc. No.: TR10235, Full Call No.: NASA TN D-620 -, Item type: Technical Report , Location: General Stacks,
------------------------- --------------------- ------ --------- ------- ------- --------- --------