External Store Airloads Prediction Technique
Author: A. R. Rudnicki (Jr.)
Publisher:
Published: 1975
Total Pages: 170
ISBN-13:
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Author: A. R. Rudnicki (Jr.)
Publisher:
Published: 1975
Total Pages: 170
ISBN-13:
DOWNLOAD EBOOKAuthor: A. R. Rudnicki (Jr.)
Publisher:
Published: 1975
Total Pages: 342
ISBN-13:
DOWNLOAD EBOOKAuthor: A. R. Rudnicki (Jr.)
Publisher:
Published: 1975
Total Pages: 122
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1975
Total Pages: 118
ISBN-13:
DOWNLOAD EBOOKPresented is an empirical method to compute six-component captive store airloads for single and multiple carriage store configurations for an arbitrary aircraft. The method has the capability for computing the basic airload and the incremental airloads due to aircraft yaw and adjacent store interference. The single carriage method was developed for the Mach range 0.5 to 2.0 while the multiple carriage method is valid for the Mach range 0.5 to 1.6. Both single and multiple carriage methods were developed for the angle of attack range -4 to +12 degrees, and the aircraft yaw angle range -8 + 8 degrees. Comparisons between predicted and experimental data show generally good agreement. The report is presented in two volumes. Volume I is the technical summary report describing the program and approach used to develop the prediction technique. Volume II, the user's manual, consists of five books.
Author: A. R. Rudnicki (Jr.)
Publisher:
Published: 1975
Total Pages: 282
ISBN-13:
DOWNLOAD EBOOKAuthor: A. R. Rudnicki (Jr.)
Publisher:
Published: 1975
Total Pages: 274
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1975
Total Pages: 279
ISBN-13:
DOWNLOAD EBOOKAuthor: A. R. Rudnicki (Jr.)
Publisher:
Published: 1975
Total Pages: 212
ISBN-13:
DOWNLOAD EBOOKAuthor:
Publisher:
Published: 1975
Total Pages: 164
ISBN-13:
DOWNLOAD EBOOKPresented is an empirical method to compute six-component captive store airloads for single and multiple carriage store configurations for an arbitrary aircraft. The method has the capability for computing the basic airload and the incremental airloads due to aircraft yaw and adjacent store interference. The single carriage method was developed for the Mach range 0.5 to 2.0 while the multiple carriage method is valid for the Mach range 0.5 to 1.6. Both single and multiple carriage methods were developed for the angle of attack range -4 to + 12 degrees and the aircraft yaw angle range -8 and +8 degrees. Comparisons between predicted and experimental data show generally good agreement. The report is presented in two volumes. Volume I is the technical summary report describing the program and approach used to develop the prediction technique. Volume II is the user's manual consisting of five separate books.
Author:
Publisher:
Published: 1975
Total Pages: 208
ISBN-13:
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